Prop Recommendations
|
|
|
- Roland Lewis
- 6 years ago
- Views:
Transcription
1 Prop Recommendations Contents Anchor Points... 2 ngines: Rotax... 4 Rotax 277: 26 HP <> 6250 Max Rpm... 4 MZ 34/35: 27 HP <> 6250 Max Rpm... 4 HIRTH F33: 28 HORSPOWR <> 6500 MAX RPM... 5 Generac: 33 HP <> 3200 Max Rpm... 5 Briggs & Stratton: 35 HP <> 3600 or 4200 Max Rpm... 6 Vanguard: 35 HP <>? Max Rpm... 6 Rotax 377: 35 HP <> 6500 Max Rpm... 7 Kawasaki 440: 38 HP <> 5000 Max Rpm... 7 HIRTH 2702: 40 HORSPOWR <> 5500 MAX RPM... 8 Rotax 447: 40 HP <> 6500 Max Rpm... 9 Rotax 503 SC: 46 HP <> 6250 Max Rpm... 9 Hirth F23: 50 HP <> 6150 Max Rpm Rotax 503 DC: 52 Hp <> 6500 Max Rpm Hirth 2704 / 3202: 55 HP <> 5500 Max Rpm MZ 202: 60 HP <> 6250 Max Rpm... 13
2 HKS 700 : 60 HP <> 6200 Max Rpm Hirth 3502: 60 HP <> 6000 Max Rpm Rotax 582: 65 HP <> 6500 Max Rpm Hirth 2706 & 3203: 65 HP <> 6200 Max Rpm Hirth 3503: 70 HP <> 6500 Max Rpm Rotax 618: 75 HP <> 6500 Max Rpm Hirth F30: 80 HP <> 5500 Max Rpm Rotax 912: 80 HP <> 5800 Max Rpm Hirth F30: 85 HP <> 5500 Max Rpm Rotax 912-ULS: 100 HP <> 5800 Max Rpm HIRTH 3701: 100 HORSPOWR <> 6000 MAX RPM HIRTH F30: 110 HORSPOWR <> 6200 MAX RPM Anchor Points specially on slow airplanes, always use ALL the potential diameter available! More climb larger prop, smaller pitch More cruise speed smaller prop, larger pitch
3 50-HP engines (503) with a 3.47: THR-bladed 70" F-model; for faster craft: 3b 65-inch B 65-HP engines (582) with a 2.60 ( ): TWO-bladed 70" F-model for faster craft: 3b 66-inch F Ideal blade tip RPM is 75% the speed of sound Larger blades ( F & B ) will cause more drag at idle / engine out giving a higher descent rate two blades have more slip at low airspeed and power loading, so they are not as good at climb or low cruise speeds. Once airspeed increases the combined drag of three blades kicks in and makes them less efficient. This does not include blade stall due to higher pitch angles for a two blade that is the same diameter. Roger THRUST: According to client; our 3-blade B w/48 at 6200RPM and GB 2.34 is developing 160lbs of static thrust AIR-SPD: You need to set a top speed limit for the F-model at about mph. The CB10 is WAY too fast to prop with the F-model, or the B. The reason is the twist. If you look at a prop for an RV or anything else that fast you'll see the prop has far more twist in it than the F-model. That twist allows air to go through the prop at high airframe speeds. Without enough twist, the inner sections of the prop will not have positive AOA at high airframe speeds. When that happens the inner sections of the prop will make drag instead of thrust. High twist allows the air to go through the prop and not make drag.
4 ngines: Rotax 20-hp 4-cyc w/rpm of 2000 at blades, recommended 3/50 (Adam Gibson) Rotax 277: 26 HP <> 6250 Max Rpm (with ng RPM: 6250) '' Blade / /53 3/ /56 3/52 3/51 arlier versions produced 26 hp (19 kw) at 6250 rpm or 38 hp (28 kw) with a tuned exhaust at 6450 rpm. The current production engine is rated at 27.5 hp (21 kw) at 6250 rpm. ratios available are 1.84, 2.05, 2.14, 2.24 and 2.34 to 1 MZ 34/35: 27 HP <> 6250 Max Rpm (with ng RPM: 6250) '' Blade / / / /53 3/47
5 /55 3/51 3/50 HIRTH F33: 28 HORSPOWR <> 6500 MAX RPM (with ng RPM: 6000) C '' Blade 1.8 Belt /50 3/ Belt /54 3/ Belt /56 3/52 2/60 3/57 3/53 Generac: 33 HP <> 3200 Max Rpm (with ng RPM: 3200) '' Blade F /54 BowFishing 3/63
6 PPC Dragonfly Briggs & Stratton: 35 HP <> 3600 or 4200 Max Rpm (with ng RPM:?) '' Blade F 1.69 IF 4200 RPM / / / / /53 3/ IF 3600 RPM / / / / / / /48-53 Vanguard: 35 HP <>? Max Rpm (with ng RPM:?) '' Blade F 1.69 IF 4200 RPM / / / / /53 3/ IF 3600 RPM / / / / / / / / /48-53
7 Rotax 377: 35 HP <> 6500 Max Rpm (with ng RPM: 6500) '' Blade F /52 3/ /56 3/ /58 3/54 3/ /60 3/55 2/ / /53 Kawasaki 440: 38 HP <> 5000 Max Rpm (with ng RPM: 5000/6500) '' Blade F if /60 3/56 2/61 3/57 3/53? if /61 3/57 2/62 3/ if /63 3/60 4/56 5/53 2/65 3/ if 6500
8 if if /62 3/ if if /63 3/60 HIRTH 2702: 40 HORSPOWR <> 5500 MAX RPM MAX PROP RPM (with ng RPM: 5500) C '' Blade /58 3/51 2/60 3/53 2/61 3/56 3/52 3/53 3/ / /64 3/ /62 4/59 2/68 3/62
9 /70 3/66 Rotax 447: 40 HP <> 6500 Max Rpm (with ng RPM: 6500) '' Blade /56 3/ /59 2/61 3/55 3/ /62 3/57 2/64 3/ /65 3/ / / /64 2/ /71 3/66 Rotax 503 SC: 46 HP <> 6250 Max Rpm (with ng RPM: 6250)
10 /52 Joe G /63 3/59 3/ /64 4/60 4/63 5/60 2/68 2/72 3/ /72
11 Hirth F23: 50 HP <> 6150 Max Rpm (with ng RPM: 6150) F 1.8 Belt /59 3/ Belt /60 2/62 3/58 4/ Belt /63 3/61 4/57 5/54 Rotax 503 DC: 52 Hp <> 6500 Max Rpm (with ng RPM: 6500) /65 3/ /58 3/ /66 3/67 WSC
12 /62 2/ /65 5/63 2/74 3/70 4/67 3/ /70* *confirmed good* 12 So 72 may be BTTR! 5/66 HIRTH 2703: 55 HORSPOWR <> 6200 MAX RPM (with ng RPM: 6200) / / /63 3/60 3/ /70 3/68
13 /72 Hirth 2704 / 3202: 55 HP <> 5500 Max Rpm (with ng RPM: 5500) /65 3/61 2/67 3/ /70 2/74 3/ / MZ 202: 60 HP <> 6250 Max Rpm (with ng RPM: 6250) C /62 4/59 3/63 2/67 3/63
14 /62 3/66 2/70 3/ HKS 700 (4-cycle - but turns like Rotax a 2-cycle?): 60 HP <> 6200 Max Rpm (with ng RPM: 6250) C /64 4/61 2/ /62 3/66 2/70 3/ /65 3/70 4/67 Hirth 3502: 60 HP <> 6000 Max Rpm (with ng RPM: 6000) C
15 /63 4/60 4/62 2/68 3/ /65 3/70 4/ /74 4/70 5/67 Rotax 582/532: 65 HP <> 6500 Max Rpm (with ng RPM: 6500) /62 2/69 3/66 4/63 2/70 3/66 4/62 5/ /64 5/61 3/68 2/74 3/68
16 4/ /65 5/63 4/69 5/66 3/72 4/69 5/ /69 3/75 4/72 5/69 Hirth 2706 & 3203: 65 HP <> 6200 Max Rpm (with ng RPM: 6200) /63 3/58 *3/60 2/65 3/61 2/ /64 3/ /70 2/75 3/72 4/69
17 /74 Hirth 3503: 70 HP <> 6500 Max Rpm (with ng RPM: 6500) C / /63 2/ /65 3/ /72 4/ /72 5/69 Rotax 618: 75 HP <> 6500 Max Rpm (with ng RPM: 6500)
18 /66 4/62 2/72 3/67 4/62 5/ /65 5/62 3/69 4/66 2/74 3/70 4/66 5/ /74 4/70 5/ HKS 700T: 80 HP <> 6200 Max Rpm (with ng RPM: 6250) C /64 4/61 5/58 2/69 4/61 5/ /62 3/66 2/72 3/68
19 5/59 4/64 5/ /70 4/69 5/71 Hirth F30: 80 HP <> 5500 Max Rpm (with ng RPM: 5500) C /64 2/68 3/ /72 3/ / /76 3/72 4/68 5/64 3/75 4/ /71
20 Rotax 912: 80 HP <> 5800 Max Rpm (with ng RPM: 5800) /65 3/69 4/66 2/72 3/70 4/66 5/63 Hirth F30: 85 HP <> 5500 Max Rpm (with ng RPM: 5500) C /62 2/69 3/ /65 2/73 3/ /65 3/ / /72 Rotax 912-ULS: 100 HP <> 5800 Max Rpm
21 (with ng RPM: 5800) Notes /65 5/67 2/75 3/73 4/70 5/ ULS on a Bushcaddy R80 3blade: dia. HIRTH 3701/3703: 100 HORSPOWR <> 6000 MAX RPM (with ng RPM: 6000) C / / /72 3/68 2/75 3/72 4/68 3/75 4/70 5/66 4/74 5/ /74
22 /75 HIRTH F30: 110 HORSPOWR <> 6200 MAX RPM (with ng RPM: 6200) /64 3/ /64 3/ / / /74
CHAPTER 9 PROPELLERS
CHAPTER 9 CHAPTER 9 PROPELLERS CONTENTS PAGE How Lift is Generated 02 Helix Angle 04 Blade Angle of Attack and Helix Angle Changes 06 Variable Blade Angle Mechanism 08 Blade Angles 10 Blade Twist 12 PROPELLERS
Beechcraft Duchess 76 Maneuver Notes
Beechcraft Duchess 76 Maneuver Notes I. Maneuver notes for Performance (AOA V), Slow Flight and Stalls (AOA VIII), Emergency Operations (AOA X), and Multiengine Operations (AOA XI) a. Maneuvers addressed:
NORMAL TAKEOFF AND CLIMB
NORMAL TAKEOFF AND CLIMB CROSSWIND TAKEOFF AND CLIMB The normal takeoff is one in which the airplane is headed directly into the wind or the wind is very light, and the takeoff surface is firm with no
Normal T/O Procedure. Short Field T/O Procedure
Normal T/O Procedure Add full power: Engine Instruments green Airspeed alive 1,000 AGL Accelerate to enroute climb 85 KIAS Complete climb check Vr = 55-60 Vy 79 KIAS Prior to Receiving T/O Clearance Complete
XI.B. Power-On Stalls
XI.B. Power-On Stalls References: AC 61-67; FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge
XI.C. Power-Off Stalls
References: FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should develop knowledge of stalls regarding aerodynamics,
Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.
![Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.](/thumbs/82/86661300.jpg "Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.")
Chapters 2 and 3 of the Pilot s Handbook of Aeronautical Knowledge (FAA-H-8083-25) apply to powered parachutes and are a prerequisite to reading this book. This chapter will focus on the aerodynamic fundamentals
Commercial Maneuvers for PA28RT-201
Commercial Maneuvers for PA28RT-201 Cruise checklist: Power 23'', 2400 RPM (23, 24) Lean mixture Fuel Pump Off (Check positive fuel pressure) Landing light Off Pre-Maneuver Checklist in the Takeoff configuration
CHAIN DRIVE Introduction Merits and demerits of chain drives Merits Demerits
70 CHAIN DRIVE Introduction Chain is used to transmit motion from one shaft to another shaft with the help of sprockets. Chain drives maintain a positive speed ratio between driving and driven components,
Report for the Submission of Data Supporting World Record Runs in the Dead Downwind Vehicle Category
Report for the Submission of Data Supporting World Record Runs in the Dead Downwind Vehicle Category Prepared by Rick Cavallaro 12 July 2010 Introduction On the 2 nd and 3 rd of July 2010, the ThinAir
Compiled by Matt Zagoren
The information provided in this document is to be used during simulated flight only and is not intended to be used in real life. Attention VA's - you may post this file on your site for download. Please
Brief Maintenance Manual DAR-Solo
Brief Maintenance Manual DAR-Solo Sofia 2009 Page: 1 TABLE OF CONTENTS Introduction 3 Limitations and safety information 4 General view of DAR-Solo prototype 7 Technical Data 8 Inspection before and after
Cessna 172 Profiles. TRAFFIC PATTERNS (Check Chart Supplement prior to flight) Index
Cessna 172 Profiles TRAFFIC PATTERNS (Check Chart Supplement prior to flight) Index When Cleared for Takeoff - Landing/Taxi lights ON Mixture-As Required Power-Check Takeoff RPM Power Climb at Vy Start
Visualized Flight Maneuvers Handbook
Visualized Flight Maneuvers Handbook For High Wing Aircraft Third Edition For Instructors and Students Aviation Supplies & Academics, Inc. Newcastle, Washington Visualized Flight Maneuvers Handbook for
NORMAL TAKEOFF PILOT TRAINING MANUAL KING AIR 200 SERIES OF AIRCRAFT
NORMAL TAKEOFF Climb-Out 1. Accelerate to 160 KIAS 2. Landing/Taxi lights: Out 3. Climb Checklist complete 1. 160 KIAS up to 10,000 ft 2. Decrease 2 KIAS per 1,000 ft above 10,000 ft to 130 KIAS at 25,000
Straight and Level. Basic Concepts. Figure 1
Basic Concepts Straight and Level This lesson should start with you asking the student what they did in the last lesson, what do they remember, and determining if they have remembered correctly. We must
The ultimate STOL aircraft
The ultimate STOL aircraft A NEW DYMAGIC DIMENSION When Shocking Dynamic and Magic Hyper STOL Performances simply meet togheter. Photo credit STEEN MADE FOR ADVENTURE The roomy, comfortable, reinforced
South African Powered Paragliding Theoretical Knowledge Test
South African Powered Paragliding Theoretical Knowledge Test Last Updated 5 February 2002 Question 1: (PTE) Explain what you understand about the Propeller Torque Effect, including its causes and effects
PRE-TEST Module 2 The Principles of Flight Units /60 points
PRE-TEST Module 2 The Principles of Flight Units 1-2-3.../60 points 1 Answer the following questions. (20 p.) moving the plane (4) upward / forward. Opposed to that is 1. What are the names of the four
Aerodynamic Control of Flexible Structures in the Natural Wind
Ian Castro 65 th Birthday Workshop, Southampton University, 28-29. 3. 12. Aerodynamic Control of Flexible Structures in the Natural Wind Mike Graham Department of Aeronautics, Imperial College London.
Cessna 172R Profiles
Cessna 172R Profiles TRAFFIC PATTERNS (Verify pattern altitude) Start your first climbing turn within 300' of pattern altitude Enter 45 degree angle to the downwind leg Depart the traffic pattern straight-out,
Student Pilot s Guide
Student Pilot s Guide The Cirrus SR22 is a remarkably simple, safe and easy aircraft to fly. Angelina Jolie flying her own Cirrus. Key Words 1. My Airplane or I ve got it - means to let go of all controls
ROAD MAP... D-1: Aerodynamics of 3-D Wings D-2: Boundary Layer and Viscous Effects D-3: XFLR (Aerodynamics Analysis Tool)
Unit D-1: Aerodynamics of 3-D Wings Page 1 of 5 AE301 Aerodynamics I UNIT D: Applied Aerodynamics ROAD MAP... D-1: Aerodynamics of 3-D Wings D-: Boundary Layer and Viscous Effects D-3: XFLR (Aerodynamics
LECTURE 18 WIND POWER SYSTEMS. ECE 371 Sustainable Energy Systems
LECTURE 18 WIND POWER SYSTEMS ECE 371 Sustainable Energy Systems 1 HISTORICAL DEVELOPMENT The first wind turbine used to generate electricity was built by La Cour of Denmark in 1891 2 HISTORICAL DEVELOPMENT
Takeoff Performance. A 1 C change in temperature from ISA will increase or decrease the takeoff ground roll by 10%.
The precise pilot does not fly by rules of thumb, axioms, or formulas. But there are times when knowledge of an approximate way to calculate things or knowledge of a simple rule can pay big dividends.
DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA
MT DIREION DE PERSONL ERONUTIO DPTO. DE INSTRUION PREGUNTS Y OPIONES POR TEM 1 TEM: 0114 TP - (HP. 03) ERODYNMIS OD_PREG: PREG20078023 (8358) PREGUNT: What is the safest and most efficient takeoff and
Uncontrolled copy not subject to amendment. Principles of Flight
Uncontrolled copy not subject to amendment Principles of Flight Principles of Flight Learning Outcome 3: Know the principles of stalling Principles of Flight Revision Questions What effect does a Trailing
New Vessel Fuel Efficient Design and Construction Considerations Medium and Long-Term Options
New Vessel Fuel Efficient Design and Construction Considerations Medium and Long-Term Options By Dag Friis Christian Knapp Bob McGrath Ocean Engineering Research Centre MUN Engineering Overview : Introduction
CIVIL AVIATION AUTHORITY SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM47 ISSUE: 11
TYPE: MAINAIR BLADE (1) MANUFACTURER: P & M Aviation Ltd, Unit B, Crawford Street, Rochdale, Lancashire, OL16 5NU (2) UK IMPORTER: - (3) CERTIFICATION: BCAR Section, Advance Issue as amended October 1988
PROCEDURES GUIDE CESSNA 172N SKYHAWK
PROCEDURES GUIDE CESSNA 172N SKYHAWK THESE PROCEDURES ARE DESIGNED TO PROVIDE STANDARDIZED METHODS UNDER NORMAL CONDITIONS. AS CONDITIONS CHANGE, THE PROCEDURES WILL NEED TO BE ADJUSTED. PASSENGER BRIEFING
DEFINITIONS. Aerofoil
Aerofoil DEFINITIONS An aerofoil is a device designed to produce more lift (or thrust) than drag when air flows over it. Angle of Attack This is the angle between the chord line of the aerofoil and the
Stability and Flight Controls
Stability and Flight Controls Three Axes of Flight Longitudinal (green) Nose to tail Lateral (blue) Wing tip to Wing tip Vertical (red) Top to bottom Arm Moment Force Controls The Flight Controls Pitch
Chain Drives. 1. As no slip takes place during chain drive, hence perfect velocity ratio is obtained
1. Introduction Chain Drives In Belt and Rope drives slipping may occur. In order to avoid slipping, steel chains are used. The chains are made up of a number of rigid links which are hinged together by
Tiger Moth basic handling notes
Tiger Moth basic handling notes by David Phillips To move the aeroplane, lift the tail by the tailplane strut, gripping as close as possible to the fuselage. The aeroplane will be neutrally balanced when
Flight Profiles are designed as a guideline. Power settings are recommended and subject to change based
MANEUVERS AND PROCEDURES Flight Profiles are designed as a guideline. Power settings are recommended and subject to change based upon actual conditions (i.e. aircraft weight, pressure altitude, icing conditions,
Gyroplane questions from Rotorcraft Commercial bank
Gyroplane questions from Rotorcraft Commercial bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter) FAA Question Number: 5.0.5.8 FAA Knowledge Code: B09 To begin a flight
DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA
MT DIREION DE PERSONL ERONUTIO DPTO. DE INSTRUION PREGUNTS Y OPIONES POR TEM 1 TEM: 0292 FLT/DSP - (HP. 03) ERODYNMIS OD_PREG: PREG20084823 (8324) PREGUNT: When are inboard ailerons normally used? Low-speed
Small Scale Wind Technologies Part 2. Centre for Renewable Energy at Dundalk IT CREDIT
Small Scale Wind Technologies Part 2 Centre for Renewable Energy at Dundalk IT CREDIT 1 Part 2 Small and large scale wind turbine technologies 2 Overview of small scale grid connected system Wind Turbine
FAA-S-ACS-6 June 2016 Private Pilot Airplane Airman Certification Standards. Task ACS Settings
FAA-S-ACS-6 June 2016 Private Pilot Airplane Airman Certification Standards Cessna 172: mixture rich, carb heat out if below the green arc. Clearing Turns all manuevers! Task ACS Settings Traffic Pattern
U.S. TSUBAKI BS/DIN ROLLER CHAIN
TSUBAKI BS/DIN ROLLER CHAIN BS/DIN Roller Chain These chains are manufactured to International Standards Organization metric dimensions (ISO 606), British Standard (BS 228), and DIN 8187. They are available
A Performanced Based Angle of Attack Display
A Performanced Based Angle of Attack Display David F. Rogers, Phd, ATP www.nar-associates.com The Problem The current angle of attack displays basically warn you about the approach to stall with yellow
Attitude Instrument Flying and Aerodynamics
Attitude Instrument Flying and Aerodynamics 2.1 TURNS 1. An airplane requires a sideward force to make it turn. a. When the airplane is banked, lift (which acts perpendicular to the wingspan) acts not
Uncontrolled copy not subject to amendment. Principles of Flight
Uncontrolled copy not subject to amendment Principles of Flight Principles of Flight Learning Outcome 1: Know the principles of lift, weight, thrust and drag and how a balance of forces affects an aeroplane
Preliminary Design Review (PDR) Aerodynamics #2 AAE-451 Aircraft Design
Preliminary Design Review (PDR) Aerodynamics #2 AAE-451 Aircraft Design Aircraft Geometry (highlight any significant revisions since Aerodynamics PDR #1) Airfoil section for wing, vertical and horizontal
Following is an incident described by the crew operating a CRJ on an early morning winter flight.
Safety Targeted Awareness Report from the ERA Air Safety Group STAR 009 V2 December 2014 Winter Operations Tailplane and Engine Fan Blade Icing Introduction FAR/JAR Part 25 transport airplanes are equipped
Single Engine Complex Training Supplement PA28R-201 Piper Arrow III (Spring 2016 Revision)
Single Engine Complex Training Supplement PA28R-201 Piper Arrow III (Spring 2016 Revision) V-speed Quick Reference V-Speed KIAS Description Airspeed Indicator Marking VSO 55 Stall speed in landing configuration
TABLE OF CONTENTS. PAC Customer Service
TABLE OF CONTENTS PROPELLERS: WHERE THE POWER MEETS THE WATER!.................................2 HOW DOES A PROPELLER WORK?.....................................................2 WHAT TO CONSIDER WHEN SHOPPING
Tecnam Eaglet Standard Operating Procedures and Maneuvers Supplement
Tecnam Eaglet Standard Operating Procedures and Maneuvers Supplement Normal Takeoff Flaps Take Off Trim set Fuel pump on Check for traffic Line up on white stripe Full power Stick should be located in
AIR FACTS The Magazine for Pilots March 1949
AIR FACTS The Magazine for Pilots March 1949 THE PIPER CLIPPER By Leighton Collins In pursuing further his long held thesis that rather than getting bigger and heavier all the time the strictly personal
PERFORMANCE MANEUVERS
Ch 09.qxd 5/7/04 8:14 AM Page 9-1 PERFORMANCE MANEUVERS Performance maneuvers are used to develop a high degree of pilot skill. They aid the pilot in analyzing the forces acting on the airplane and in
COCKPIT STRAIGHT AND LEVEL FLIGHT, CLIMBS AND GLIDES. By Harold Holmes (EAA ), CPI 1038 Inverrary Lane Deerfleld, IL 60015
COCKPIT STRAIGHT AND LEVEL FLIGHT, CLIMBS AND GLIDES By Harold Holmes (EAA 220238), CPI 1038 Inverrary Lane Deerfleld, IL 60015 J. HE OBJECTIVE OF straight and level night as stated in the Maldon Books
Impact of Upcoming Stall/Upset Requirements in the U.S.
Impact of Upcoming Stall/Upset Requirements in the U.S. Federal Aviation Administration Robert Burke Jeffery Schroeder World Aviation Training Conference April 19, 2016 1 Main points Implementing regulations
Vessel Modification and Hull Maintenance Considerations Options & Pay Back Period or Return On Investments
Vessel Modification and Hull Maintenance Considerations Options & Pay Back Period or Return On Investments By Dag Friis Christian Knapp Bob McGrath Ocean Engineering Research Centre MUN Engineering 1 Overview:
Club Fitting Report. (c) Swing Labs, LLC. All Rights Reserved. This report created using Swing Labs Club Fitting Software.
Club Fitting Report Golfer: Mark Golfer ID: # 172116 Date: Type: Location: Fitter: October 10, 2017 06:43 PM GMT Club Compare - Dashboard Driver Fitting Swing Labs 732 Cable Beach Lane suite 1 North Palm
C-130 Reduction in Directional Stability at Low Dynamic Pressure and High Power Settings
C-130 Reduction in Directional Stability at Low Dynamic Pressure and High Power Settings The C-130 experiences a marked reduction of directional stability at low dynamic pressures, high power settings,
Aviation Merit Badge Knowledge Check
Aviation Merit Badge Knowledge Check Name: Troop: Location: Test Score: Total: Each question is worth 2.5 points. 70% is passing Dan Beard Council Aviation Knowledge Check 1 Question 1: The upward acting
Design and Analysis of Rotary Lawn Mower
Design and Analysis of Rotary Lawn Mower Vivek P Revi Vishnu N V Akhil K A Rohith P Kevin Rozario Abstract- KAMCO Industries, Athani, India is a reputed industry undertaken by Kerala state government producing
Outbound Progress Report Choosing an Engine:
Outbound Progress Report 14 10-25-17 Choosing an Engine: A new design starts with an engine choice, and for the Outbound that was the Titan 340. No doubt this will prove a very viable and well fitted engine.
Climbs, descents, turns, and stalls These are some of the maneuvers you'll practice, and practice, and practice By David Montoya
Climbs, descents, turns, and stalls These are some of the maneuvers you'll practice, and practice, and practice By David Montoya Air work stalls, steep turns, climbs, descents, slow flight is the one element
Jet Propulsion. Lecture-17. Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati
Lecture-17 Prepared under QIP-CD Cell Project Jet Propulsion Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1 Lift: is used to support the weight of
WHAT IS GLIDER? A light engineless aircraft designed to glide after being towed aloft or launched from a catapult.
GLIDER BASICS WHAT IS GLIDER? A light engineless aircraft designed to glide after being towed aloft or launched from a catapult. 2 PARTS OF GLIDER A glider can be divided into three main parts: a)fuselage
1 In The Biginning. Nice Air Operation Procedure Cessna 172
1 In The Biginning Check how many hours remains for next 100h inspection and check squawk before take airplane. Perform pre-flight inspection using check list. Report to the front desk if you need fuel,
6.0 OPERATING CONDITIONS. 6.1 Jet Engine Exhaust Velocities and Temperatures 6.2 Airport and Community Noise
6. OPERATING CONDITIONS 6.1 Jet Engine Exhaust Velocities and Temperatures 6.2 Airport and Community Noise DISTANCE FROM AIRPLANE CL 8 1 PLAN 4 4 NOTES: 1. ENGINE CF6-8C2 2. THESE CONTOURS ARE TO BE USED
How Does A Wind Turbine's Energy Production Differ from Its Power Production? 1
Siting Wind Power: Wind Power Curves & Community Considerations (Teacher Notes) (Assessing the Feasibility of Wind Power for Pennsylvania) Notes on Part 1 A Beaufort scale is included on the next page
HEIGHT VELOCITY CURVE for GYROPLANES
HEIGHT VELOCITY CURVE for GYROPLANES - By Greg Gremminger This article is an update to the original article on the subject we had published in Rotorcraft several years ago. The subject is an important
Introducing The Gemma One
Introducing The Gemma One The Gemma One is a new generation clean vessel: a practical, safe, conservatively styled, amenity-rich, and highly automated boat that can be 100% powered by renewable energy,
Chain Drives ELEMEN MESIN II
Chain Drives ELEMEN MESIN II Introduction Belt and rope drives slipping may occur To avoid slipping Chains The chains are made up of number of rigid links which are hinged together by pin joints in order
Basic Fluid Mechanics
Basic Fluid Mechanics Chapter 7B: Forces on Submerged Bodies 7/26/2018 C7B: Forces on Submerged Bodies 1 Forces on Submerged Bodies Lift and Drag are forces exerted on an immersed body by the surrounding
Detailed study 3.4 Topic Test Investigations: Flight
Name: Billanook College Detailed study 3.4 Topic Test Investigations: Flight Ivanhoe Girls Grammar School Questions 1 and 2 relate to the information shown in the diagram in Figure 1. z Question 1 y Figure
Aerobatic Trimming Chart
Aerobatic Trimming Chart From RCU - Chip Hyde addresses his view of Engine/Motor thrust. I run almost no right thrust in my planes and use the thottle to rudd mix at 2% left rudd. to throttle at idle.
Part I: Blade Design Methods and Issues. James L. Tangler
Part I: Blade Design Methods and Issues James L. Tangler Senior Scientist National Renewable Energy Laboratory National Wind Technology Center Steady-State Aerodynamics Codes for HAWTs Selig, Tangler,
Give Wings to Imagination
Give Wings to Imagination Water rocket uses water as a propellant. PRINCIPLE It is based on the NEWTON S THIRD LAW OF MOTION. For a simple model, water rocket consists of a bottle having water above
LAPL/PPL question bank FCL.215, FCL.120 Rev PRINCIPLES OF FLIGHT 080
LAPL/PPL question bank FCL.215, FCL.120 Rev. 1.7 11.10.2018 PRINCIPLES OF FLIGHT 080 1 Density: Reduces with temperature reduction. Increases with altitude increase. Reduces with altitude increase. Is
C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory
ROAD MAP... AE301 Aerodynamics I UNIT C: 2-D Airfoils C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory AE301 Aerodynamics I : List of Subjects
Advanced Stalling. L = CL ½ ρ V 2 S. L = angle of attack x airspeed. h L = angle of attack x h airspeed. Advanced Manoeuvres
Advanced Manoeuvres Advanced Stalling This Advanced Stalling lesson covers the factors that affect the observed airspeed and nose attitude at the stall. Although the aeroplane always stalls when the aerofoil
Aircraft - Very Heavy Lift at Very Low Cost
Aircraft - Very Heavy Lift at Very Low Cost Stephen Funck This is a span loader for standard shipping containers. The design goal is the lowest cost per ton / mile. Low wing loading allows for low flight
See the diagrams at the end of this manual for judging position locations.
Landing Events Penalties General Judges should use airport diagrams, satellite pictures or other means to determine, as accurately as possible, assessments of landing pattern penalties. Judges should be
Introduction INDEX. INTRODUCTION HSE
Introduction INDEX SECTION PAGE INTRODUCTION ORDERING CODE GLOSSARY MOTOR OPTION TECHNICAL SE SE3 / SE5 SE7 / S7 SE9 / S9 SE12 / S12 SE14 / S14 SE14-2 / S14-2 SE17 / S17 SE17-2 / S17-2 SE21 / S21 SE21-2
Understanding your propeller
gear Understanding your propeller Choosing the correct propeller for your boat involves complex formulae and an understanding of how a prop works but in the end getting best performance still boils down
GENERAL AVIATION - CLIMBING
GENERAL AVIATION - CLIMBING This tutorial follows on from the normal take off and will address climbing. The techniques described here are again generic in nature and may yield slightly different results
Exploration Series. AIRPLANE Interactive Physics Simulation Page 01
AIRPLANE ------- Interactive Physics Simulation ------- Page 01 What makes an airplane "stall"? An airplane changes its state of motion thanks to an imbalance in the four main forces acting on it: lift,
Flying Wings. By Henry Cole
Flying Wings By Henry Cole FLYING WINGS REPRESENT THE THEORETICAL ULTIMATE IN AIRCRAFT DESIGN. USE THESE IDEAS, AVAILABLE AFTER A YEAR, OF RESEARCH, TO DEVELOP PRACTICAL MODELS. The rubber version of this
A103 AERODYNAMIC PRINCIPLES
A103 AERODYNAMIC PRINCIPLES References: FAA-H-8083-25A, Pilot s Handbook of Aeronautical Knowledge, Chapter 3 (pgs 4-10) and Chapter 4 (pgs 1-39) OBJECTIVE: Students will understand the fundamental aerodynamic
MANEUVERS GUIDE. Liberty Aerospace 1383 General Aviation Drive Melbourne, FL (800)
MANEUVERS GUIDE Liberty Aerospace 1383 General Aviation Drive Melbourne, FL 32935 (800) 759-5953 www.libertyaircraft.com Normal/Crosswind Takeoff and Climb 1. Complete the runup and before takeoff checklist.
RESULTS FROM PARACHUTE SEA ANCHOR DRAG TESTS FOR A SPACE CAPSULE, Jan. 10, 2013
FIORENTINO Technical Report FPA-152 Report Prepared for: America s next generation of spacecraft A spacecraft can be a diameter of 16.5-foot and weigh 18,000 lbs. at splashdown. When the parachute sea
ProKat 2860 Cuddy Cabin My Kitty Kat
ProKat 2860 Cuddy Cabin My Kitty Kat Make: Model: Length: ProKat 2860 Cuddy Cabin 29 ft 1 in Price: $ 95,000 Year: 2007 Condition: Used Boat Name: Hull Material: Draft: Number of Engines: 2 Fuel Type:
ANNEX TO TYPE CERTIFICATE No. ULL - 07 / 2003 a
Letecká amatérská asociace ČR, Light Aircraft Association CR Ke Kablu 289, 102 00 Praha 10, Hostivař tel: sekretariát 271 085 270 fax: 27 10 85 596 e-mail: laacr@laacr.cz http://www.laacr.cz Type certificate
To learn how to recognize and recover from a loss of directional control caused by an asymmetrical thrust condition at low airspeed.
V MC Demonstration Area XIV, Task E Revised 2015-08-13 Objective To learn how to recognize and recover from a loss of directional control caused by an asymmetrical thrust condition at low airspeed. Elements
Agenda for May 4 th Meeting Marple Newtown Library, 7:30 pm
The Flightline Volume 34,Issue5 Newsletter of the Propstoppers RC Club AMA 1042 May 2004 Editorial: Field Fix Up Matters Well, the Sleighton Field fix up day was washed out but Dick Seiwell and Bob Crowell
EXAMPLE MICROLIGHT AIRCRAFT LOADING CALCULATIONS
1. Introduction This example loads report is intended to be read in conjunction with BCAR Section S and CS-VLA both of which can be downloaded from the LAA webpage, and the excellent book Light Aircraft
CHAPTER 1 - PRINCIPLES OF FLIGHT
CHAPTER 1 - PRINCIPLES OF FLIGHT Reilly Burke 2005 INTRODUCTION There are certain laws of nature or physics that apply to any object that is lifted from the Earth and moved through the air. To analyze
POWERED FLIGHT HOVERING FLIGHT
Once a helicopter leaves the ground, it is acted upon by the four aerodynamic forces. In this chapter, we will examine these forces as they relate to flight maneuvers. POWERED FLIGHT In powered flight
Aerodynamics. A study guide on aerodynamics for the Piper Archer
Aerodynamics A study guide on aerodynamics for the Piper Archer Aerodynamics The purpose of this pilot briefing is to discuss the simple and complex aerodynamics of the Piper Archer. Please use the following
XI.D. Crossed-Control Stalls
References: FAA-H-8083-3; POH/AFM Objectives Key Elements Elements Schedule Equipment IP s Actions SP s Actions Completion Standards The student should understand the dynamics of a crossed-control stall
Quintic Ball Roll Key Parameters
Quintic Ball Roll Key Parameters How to interpret the numbers... www.quinticballroll.com 1. Face Angle & Start Direction 2. Clubhead Twist 3. Ball Speed & Pace Control 4. Launch Angle 5. Spin & Roll Key
Mountain Fury Mountain Search Flying Course Syllabus
Mountain Fury Mountain Search Flying Course Syllabus Goals 1. Pilots who complete this program will be able to perform with precision and confidence all of the tasks and flight maneuvers required for safe
ABS/BPPP Performance Worksheet: Baron/Travel Air Pilots
ABS/BPPP Performance Worksheet: Baron/Travel Air Pilots This worksheet is the homework for BPPP Initial pilots to complete before their BPPP flight. It s designed to help the pilot develop a deep understanding
How to fly a powered parachute
How to fly a powered parachute 07-19-06 All rights reserved. No portion of this book may be reproduced or distributed without the expressed written permission of Oregon Aircraft Design LLC. By Bill Larson
WHERE THE POWER MEETS THE WATER!
WHERE THE POWER MEETS THE WATER! Choosing the right propeller is the single most important decision you can make to get the best performance from your boat and outboard! Propeller choice can affect boat
BS Conveyor Chain - Hollow Bearing Pin Chain
S onveyor Hollow earing in This chain has all the bearing pin hollow. The hollow bearing type chain gives easy facility for fixing attachments to outer links by bolting through the hollow bearing pins.