PERFORMANCE VS INTERCEPTOR EXTENSION

Similar documents
ZIPWAKE DYNAMIC TRIM CONTROL SYSTEM OUTLINE OF OPERATING PRINCIPLES BEHIND THE AUTOMATIC MOTION CONTROL FEATURES

Interceptors in theory and practice

Stability and Flight Controls

No Description Direction Source 1. Thrust

Uncontrolled copy not subject to amendment. Principles of Flight

CHAPTER 9 PROPELLERS

Ship Resistance and Propulsion Prof. Dr. P. Krishnankutty Ocean Department Indian Institute of Technology, Madras

The salient features of the 27m Ocean Shuttle Catamaran Hull Designs

Winnipeg Headingley Aero Modellers. Things About Airplanes.

Trim and Stabilisation systems NEXT GENERATION IN BOAT CONTROL.

V mca (and the conditions that affect it)

The Academy of Model Aeronautics ALPHA: Potential Energy Background Information for the Teacher

This lesson will be confined to the special case of ships at rest in still water. Questions of motions resulting from waves are not considered at

Aerodynamic Terms. Angle of attack is the angle between the relative wind and the wing chord line. [Figure 2-2] Leading edge. Upper camber.

Figure 1 Figure 1 shows the involved forces that must be taken into consideration for rudder design. Among the most widely known profiles, the most su

II.E. Airplane Flight Controls

What happens to a fluid (water or air) when it moves from entering a wide opening to entering a narrow opening?

Conventional Ship Testing

Aerodynamics Principles

Long and flat or beamy and deep V-bottom An effective alternative to deep V-bottom

Advanced Aerobatic Airplane Guidelines

AE Dept., KFUPM. Dr. Abdullah M. Al-Garni. Fuel Economy. Emissions Maximum Speed Acceleration Directional Stability Stability.

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA

THEORY OF WINGS AND WIND TUNNEL TESTING OF A NACA 2415 AIRFOIL. By Mehrdad Ghods

Detailed study 3.4 Topic Test Investigations: Flight

CRITERIA OF BOW-DIVING PHENOMENA FOR PLANING CRAFT

Parametric Study of the Effects of Trim Tabs on Running Trim and Resistance of Planing Hulls

Study on Resistance of Stepped Hull Fitted With Interceptor Plate

A HYDRODYNAMIC METHODOLOGY AND CFD ANALYSIS FOR PERFORMANCE PREDICTION OF STEPPED PLANING HULLS

Preliminary Design Review (PDR) Aerodynamics #2 AAE-451 Aircraft Design

Optimist Tuning Guide

1. A tendency to roll or heel when turning (a known and typically constant disturbance) 2. Motion induced by surface waves of certain frequencies.

PRODUCT KNOWLEDGE INFORMATION SHEETS PERFORMANCE FEATURES

Exam Unit 5: Motion and Forces

XI.C. Power-Off Stalls

Straight and Level. Basic Concepts. Figure 1

Fig. I Z? Fig. 4. Fig. 2. Fig. 3. Aug. 5, ,459,146. ~.aml < (qg'..-m~ ~~tw~ W,LLtI4M C. PRIOR. Filed May 19, Sheets-SheAt 1 ATTORNEYS.

(12) United States Patent

Reliable Speed Prediction: Propulsion Analysis and a Calculation Example

Flying High. HHJS Science Week Background Information. Forces and Flight

Preliminary design of a high-altitude kite. A flexible membrane kite section at various wind speeds

AUTOMATIC FLOW CARTRIDGES. Competition Analysis Not All Automatics Are Created Equal

Flightlab Ground School 7. Longitudinal Dynamic Stability

COURSE OBJECTIVES CHAPTER 9

PRE-TEST Module 2 The Principles of Flight Units /60 points

Vessel Modification and Hull Maintenance Considerations Options & Pay Back Period or Return On Investments

J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology.

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA

Figure 8: Looking Down on a Three Thruster Vehicle

Aerodynamic Analysis of a Symmetric Aerofoil

A Study on Roll Damping of Bilge Keels for New Non-Ballast Ship with Rounder Cross Section

Planing Hull Resistance Calculation The CAHI Method. SNAME Greek Section 13 October 2016 P. G. Alourdas

wind wobble unstable

XI.B. Power-On Stalls

Journal of Naval Architecture and Marine Engineering December,

A103 AERODYNAMIC PRINCIPLES

X-29 Canard Jet. A Simple Depron Foam Build.

Stability and Computational Flow Analysis on Boat Hull

It should be noted that the symmetrical airfoil at zero lift has no pitching moment about the aerodynamic center because the upper and

PEMP ACD2501. M.S. Ramaiah School of Advanced Studies, Bengaluru

COMPARATIVE ANALYSIS OF CONVENTIONAL AND SWATH PASSENGER CATAMARAN

Designing a Model Rocket

THE AIRCRAFT IN FLIGHT Issue /07/12

Three New Concepts of Multi-Hulls

Bench Trimming A Stunt Ship

Multihull Preliminary Stability Estimates are Fairly Accurate

An Investigation into the Capsizing Accident of a Pusher Tug Boat

ATPL Principles of Flight - deel 2

Aircraft Stability and Performance 2nd Year, Aerospace Engineering. Dr. M. Turner

Kinematics-Projectiles

Windmills using aerodynamic drag as propelling force; a hopeless concept. ing. A. Kragten. April 2009 KD 416

SEMI-SPAN TESTING IN WIND TUNNELS

Comparing GU & Savier airfoil equipped half canard In S4 wind tunnel (France)

PRINCIPLES OF FLIGHT

Design of high-speed planing hulls for the improvement of resistance and seakeeping performance

Hydrostatics and Stability Dr. Hari V Warrior Department of Ocean Engineering and Naval Architecture Indian Institute of Technology, Kharagpur

Four forces on an airplane

Subsonic wind tunnel models

HIGH ALTITUDE AERODYNAMICS

The Physics of Water Ballast

Parasite Drag. by David F. Rogers Copyright c 2005 David F. Rogers. All rights reserved.

BRONZE LECTURES. Slides on bayriver.co.uk/gliding

ROAD MAP... D-1: Aerodynamics of 3-D Wings D-2: Boundary Layer and Viscous Effects D-3: XFLR (Aerodynamics Analysis Tool)

The Usage of Propeller Tunnels For Higher Efficiency and Lower Vibration. M. Burak Şamşul

AERODYNAMICS I LECTURE 7 SELECTED TOPICS IN THE LOW-SPEED AERODYNAMICS

The kayak must be moving at a reasonable speed. Fully rotate the body so that both hands are out over the side.

Practice Test: Vectors and Projectile Motion

Aerodynamics. A study guide on aerodynamics for the Piper Archer

Chapter 2 Hydrostatics and Control

Table of Contents. Career Overview... 4

LONGITUDINAL ACTIVE STABILITY: KEY ISSUES FOR FUTURE LARGE TRANSPORT AIRCRAFT

Analysis of the Z-wing configuration

SECOND ENGINEER REG III/2 NAVAL ARCHITECTURE

AIRCRAFT PRIMARY CONTROLS A I R C R A F T G E N E R A L K N O W L E D G E

AF101 to AF109. Subsonic Wind Tunnel Models AERODYNAMICS. A selection of optional models for use with TecQuipment s Subsonic Wind Tunnel (AF100)

Properties of Water Affect Locomotion

Brief Introduction to a Bionic Lizard Flywheel Planing Craft. XI-YI High Speed Craft Bionic Science & Technology Ltd XYL Shanghai China

STABILITY OF MULTIHULLS Author: Jean Sans

Propellers and propulsion

OPTIMISATION OF HYDROFOIL-SUPPORTED-PLANING CATAMARANS

Transcription:

PERFORMANCE VS INTERCEPTOR EXTENSION Misleading information is circulating that claims interceptors with a large stroke and small span are better than Zipwake s wide span interceptors with a smaller stroke. The following diagrams show this information to be misleading. Indeed, it is always better from a drag point of view to generate lift using as wide a span as possible. Compare flight long, thin wings mean low drag. There is no question short interceptors in combination with large interceptor extension generates the greater lift given restricted interceptor length. However, the amount of lift does not vary linearly; rather the ratio falls off with increasing interceptor extension. For example, increasing interceptor extension from mm to mm (67 percent) only results in a theoretical lift increase of 29 percent (less in a real-world installation). Interceptor drag, on the other hand increases by 43 percent, showing that the interceptor lift-todrag ratio decreases with increasing interceptor extension. In other words, there can be no doubt that large interceptor extension with a small interceptor span in effect makes the interceptor act as a brake. When comparing equal lift forces, a small interceptor extension combined with a large span by making better use of the boat s beam is by far the best alternative with regards to drag. Significant speed gains can then be achieved, whereas the drag resulting from large extensions/small spans can actually cancel the positive effect on hull resistance from operation at a more favorable trim. It s why people note that in identical boats where one is fitted with Zipwake and the other with larger stroke interceptors the same or even higher speed is often achieved by the Zipwake boat. With regard to roll damping, it appears better at first glance to have as large a lift force and moment arm as possible. However, there is no significant difference in the moment arm of a short interceptor mounted close to the chine and a somewhat longer one. Drag, on the other hand, increases most significantly, which means the probable speed loss in a seaway might well outweigh the positive effects of reduced roll motion. Moreover, applying large interceptor lift for roll control on any planing craft with normal deadrise will inherently impose a significant side force that tends to have an undesirable effect on yaw and autopilot performance. Thus if large roll damping is essential, it may be better to opt for moderate interceptor lift and combine it with a roll motion control system that does not affect course keeping, such as a gyroscopic stabilizer.

Interceptor Lift @ Equal Span 2.5 Interceptor Lift dl/dl Interceptor Area (span x extension) 2 Interceptor extension 1.5 58% 29% 1 67% 1% 0.5 0 0 10 20 40 60 70 80 90 100 Based on ideal 2D flow of flat planing surface with interceptor. 3D effects tend to degrade lift generation, e.g. large interceptor extension in combination with a small interceptor span effectively makes the interceptor act as a brake.

Interceptor Drag @ Equal Lift 2.5 Interceptor Drag dd/dd Interceptor Area (span x extension) 2 1.5 Interceptor extension 43% 91% 1 67% 1% 0.5 0 0 10 20 40 60 70 80 90 100 Based on ideal 2D flow of flat planing surface with interceptor. 3D effects tend to degrade lift generation, e.g. large interceptor extension in combination with a small interceptor span effectively makes the interceptor act as a brake.

Boat Hydrodynamic Resistance @ Equal Interceptor Lift Displacement Aft trim, no interceptors Resistance 1. Interceptor Drag Extension mm mm Optimum trim by weight shift, no interceptors Planing Boat speed

Speed Gain @ Equal Interceptor Lift Resistance & Thrust Displacement Thrust curve, constant shaft power Speed gain Extension mm mm Aft trim, no interceptors Optimum trim by weight shift, no interceptors Planing Boat speed

Roll Moment Arm @ Equal Interceptor Lift Side force The increase in roll moment arm (H) by an interceptor with large extension-to-span ratio is limited whereas the trade-off in drag is substantial. In the above example, interceptor-induced drag increases by 91 % while roll moment only increases by 15 %. Moreover, applying large interceptor lift for roll control on any planing craft with ordinary deadrise will inherently impose significant side force that tends to have an undesirable effect on yaw motion and autopilot performance. Thus if large roll damping is essential, it may be better to settle for moderate interceptor lift and combine it with a roll motion control system that does not affect course keeping, e.g. a gyroscopic stabilizer.