Slider Drag Cancellation: Another Cause of Hard Parachute Openings

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

Aerodyne Flight Recommendations

MAN-032 Rev 0. Performance Designs Zero Packing Manual

2018 Skydiver s Information Manual Summary of Changes

Wingsuit Owners Manual

Performance Characteristics

WHAT IS GLIDER? A light engineless aircraft designed to glide after being towed aloft or launched from a catapult.

PRINCIPLES OF FLIGHT

Learning Objectives. Key Concepts: Momentum, Pressure, Aerodynamic Forces

Aerodynamics Principles

The Fly Higher Tutorial IV

Exploration Series. MODEL ROCKET Interactive Physics Simulation Page 01

Uncontrolled copy not subject to amendment. Principles of Flight

No Description Direction Source 1. Thrust

Principles of glider flight

A-License Information Packet

9-Cell MAIN CANOPIES

II.E. Airplane Flight Controls

WATER ROCK. Lawndart The rocket goes straight up and comes down nose first at high speed. Disadvantages

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

Questionnaire for the theoretical part of education in skydiving. Aerodynamics

Principles of glider flight

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

XI.C. Power-Off Stalls

Accelerated Freefall Program Cushing Airport 4 West Airport Road Cushing, OK 74023

Student Training Program

Stability and Flight Controls

Methods The experiments were carried out in the wind tunnel in the Air physics laboratory at the Engineering Centre Bygholm as shown in figure 1.

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

Aero Club. Introduction to Flight

Detailed study 3.4 Topic Test Investigations: Flight

CHAPTER 1 - PRINCIPLES OF FLIGHT

IAF Level 3 Category B

PYP 001 First Major Exam Code: Term: 161 Thursday, October 27, 2016 Page: 1

CIRCLING THE HOLIGHAUS WAY -

CHAPTER 9 PROPELLERS

MiSP Force and Gravity Worksheet #3. Name Date

Lesson: Pitch Trim. Materials / Equipment Publications o Flight Training Manual for Gliders (Holtz) Lesson 4.4 Using the Trim Control.

Exercise on Projectile Motion (Unit-III)

SMART RESERVE PACKING MANUAL

LAPL(A)/PPL(A) question bank FCL.215, FCL.120 Rev PRINCIPLES OF FLIGHT 080

BIOMECHANICAL MOVEMENT

The Aerodynamic Drag of Parafoils

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

Design and Integration of a Mechanical Aircraft Control System Mixer for Ruddervator Surfaces Advanced Tech Engineering, Inc.

1.2 THE TRADITIONAL METHOD

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

PRE- JUMP TRAINING (T-11 Heavy)

POWERED FLIGHT HOVERING FLIGHT

Category D Training Aid. All training to be conducted by instructors of the:

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

Nitro Rigging Wingsuit Course

DYNAMICS PROBLEM SOLVING

Transcript for the BLOSSMS Lesson. An Introduction to the Physics of Sailing

STABILITY OF MULTIHULLS Author: Jean Sans

EXPERIMENTAL ANALYSIS OF FLOW OVER SYMMETRICAL AEROFOIL Mayank Pawar 1, Zankhan Sonara 2 1,2

XI.B. Power-On Stalls

PILOT S HANDBOOK of Aeronautical Knowledge AC61-23C

Leg Pouch Pilot Chute System

Medium, Climbing and Descending Turns

The Metric Glider. By Steven A. Bachmeyer. Aerospace Technology Education Series

REAL LIFE GRAPHS M.K. HOME TUITION. Mathematics Revision Guides Level: GCSE Higher Tier

School of Engineering & Technology University of Hertfordshire Hatfield, AL10 9AB. Wind Tunnel Testing of Crossgrip TPO Roof Walkway Matting

Lesson Plan: Bernoulli s Lift

A103 AERODYNAMIC PRINCIPLES

Lesson: Airspeed Control

Figure 1. Outer dimensions of the model trucks.

Using SHRP 2 s NDS Video Data to Evaluate the Impact of Offset Left-Turn Lanes on Gap Acceptance Behavior Karin M. Bauer & Jessica M.

5. A bead slides on a curved wire, starting from rest at point A in the figure below. If the wire is frictionless, find each of the following.

Flight Control Systems Introduction

Visualization: Mind over Body

V mca (and the conditions that affect it)

Chapter 3: Aircraft Construction

A Next Generation Self- Locating Datum Marker Buoy

Drag Divergence and Wave Shock. A Path to Supersonic Flight Barriers

Homework Exercise to prepare for Class #2.

USER MANUAL. Contents YOU MUST READ THIS MANUAL BEFORE DOING ANYTHING WITH YOUR SQUIRREL EQUIPMENT

Category E Training Aid. All training to be conducted by instructors of the:

TAKEOFF & LANDING IN ICING CONDITIONS

Newton s Laws of Motion

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

Journal of Applied Fluid Transients, Vol 1-1, April 2014 (3-1)

PRE-JUMP FOR FORT BRAGG UNITS OCTOBER 2016

Winnipeg Headingley Aero Modellers. Things About Airplanes.

6C Science Fair Knowledge

Earthquake Waves. Purpose: To give students a visual example, using a slinky, of how an energy wave propagates through the Earth.

Where no fly has gone before...

PRE- JUMP TRAINING (T-11)

It is also possible to make a more traditional version of the design - which I call Easy Glider - which can be launched by hand in the normal way.

USER MANUAL. Before you BASE, Skydive. Please read this carefully before doing anything with your new wingsuit.

When centered riders turn inwards. Prepare to pass in suicide charge through the center of each space.

RESERVE CANOPY OWNER S GUIDE

Aerodynamic Analysis of a Symmetric Aerofoil

Millennial Walker A multi-functional, elderly assistance walker with improved posture, comfort, and folding capabilities.

ENGINEERing challenge workshop for science museums in the field of aeronautic engineering

Dragon In Flight (Version 2.5) By Charles Esseltine.

Ermenek Dam and HEPP: Spillway Test & 3D Numeric-Hydraulic Analysis of Jet Collision

Give Wings to Imagination

USER MANUAL PLEASE READ THIS CAREFULLY BEFORE DOING ANYTHING WITH YOUR NEW WINGSUIT CONTENTS

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

Transcription:

Slider Drag Cancellation: Another Cause of Hard Parachute Openings By J. Potvin and G. Peek (version 01-08-08)

Background On rare occasions the ram-air parachute wings + used in skydiving open very quickly, and in manners that generate high opening loads. In some cases, these openings have been hard enough to cause serious injuries. Several mechanisms have been proposed to explain such events, including: - slider rebound - off-staged deployments - unsual canopy and slider folding/packing We wish to suggest another mechanism which, either on its own or along with the above mechanisms, will also lead to very hard openings: Slider Drag Cancellation (or SDC ) + also called parafoils

What is Slider Drag Cancellation? Succinctly, SDC is a condition that is: - being created at the very beginning of inflation - generating high pressure areas above and below the slider s surface - impeding the slider s hability to remain at the top of the suspension lines thereby facilitating bottom skin spreading; bottom skin spreading is an extremely rapid inflation mode that generates high opening loads

In the next few slides: 1. How does a slider work in nominal openings? 2. How can slider drag be cancelled? 3. How to reduce the occurrence of SDC? 4. Concluding remarks

1. How does a slider work in nominal openings?

Reality check: parafoils do need inflation control devices for soft openings Typically, inflation control devices such as sliders lengthen the duration of inflation (and canopy expansion), which in turns reduces the magnitude of the opening shock. Without sliders, the opening would be very fast and feel very hard. Figure 1 (next slide) shows that the maximum opening forces sustained during the nominal openings of slider-reefed skydiving canopies are at about 3-5 g s Without sliders such canopies sustain maximum opening forces in the range of 10 to 15 g s (and even more see figure 1 again)

Slider decent End of opening Figure 1. Seven-cell parafoil (200ft 2 ) opening without a slider (left), versus a nine-cell parafoil (230ft 2 ) opening with a slider (right). Force expressed in g s. The two openings took place at similar speeds (120 150 fps -approx.) and weights (160 lbs approx.). The jagged curves correspond to load cell measurements, and the continuous curves to inflation models created by the authors.

Why do parafoils open hard without opening-control devices? The opening dynamics of a ram-air wing is controlled by two processes: - The air entering the cells through the leading edge inlets (i.e. cell inflation) - The span-wise spreading action of the airstream hitting the bottom skin of the canopy, a process caused by the wing s anhedral and stabilizers (this is the bottom skin spreading event mentioned previously) See figure 2 next slide

Canopy bottom skin & stabilizer Cells and cell inlets Air entering the cells; causes cell inflation stabilizers Air pushing against the bottom skin Suspension lines Air pushing the bottom skin and stabilizers; causes bottom skinspreading Side view of canopy View of the leading edge Figure 2. Airstream patterns around an inflating parafoil, at the very beginning of the inflation process (no slider)

But! Cell inflation is a much slower process than bottom-skin spreading. A canopy opening without a slider will do so via the bottom-skin opening process, and be fully extended before the cells had any chance to fill up with air. Because of the great swiftness of bottom skin-spreading, the overall canopy opening process generates large forces on the jumper. The main function of a slider is to suppress bottom skin -spreading, leaving the canopy expansion process exclusively to cell inflation.

Ram-air wings equipped with sliders will open more slowly (and more softly) for the following reasons: (see figures 3 and 4 next slide) - During the early part of inflation, the oncoming airstream keeps the slider at the very top of the suspension lines, being pushed against the canopy by it s own drag - The presence of the slider at that location provides a constraint that supresses bottom-skin spreading; canopy expansion is now pretty much controlled by cell inflation a much slower process - As cell inflation continues, there is a build-up of pressure inside the cells, which continues until the wing is pressurized enough to overcome the constraint of the slider; it is at this moment that the slider begins its motion down the suspension lines - By the time of slider-descent, the parachute-jumper system has substancially decelerated so that when the canopy spread fully, the parachute s drag force is much lower

Figure 3. Opening sequence of a slider-reefed parafoil opening in a nominal fashion

Figure 4. Forces applied on a typical slider, during slider-descent

How is slider drag generated? - See figure 5 (next slide) - Note the high-pressure area under the slider, caused by the oncoming airstream - Note the low-pressure area immediately above the slider, but the under canopy bottom skin, created by the dead air between slider and canopy bottom skin (note: there might be actual airflow there more on this later) - The difference in (total) pressure between the top and bottom pressure areas is what creates slider-drag

Canopy bottom skin & stabilizer Rear gap between slider & canopy bottom skin Cells and cell inlets Air entering cells Air pushing slider upwards Side view of canopy High pressure below slider stabilizer Lower pressure above slider (dead air) slider Front view Front gap between slider and bottom skin Figure 5. Airstream patterns during nominal openings

2. How can slider drag be cancelled?

SDC is caused by the airstream penetrating the area bewteen the canopy bottom skin and slider surface, from both sides i.e. through mostly the rear and front gaps + see figure 6 (next slide) High pressure ensues from the collision of both flows, and cancels the effect of the high pressure created by the relative wind hitting the slider from below - hence slider drag cancellation Without slider-drag, drag, the down-pushing force provided by the lines fanning out of the slider (and generated by span- spreading) is unopposed see figure 4, above; the slider thus moves downwards very quickly, almost as if the canopy had no slider to begin with + Note: Penetration may be also facilitated by the down-curvature of the canopy tail corners

Canopy bottom skin & stabilizer Air entering cells Air pushing slider upwards Air flowing in between bottom skin and slider top, through front and rear gaps, followed by pressure buildup there Figure 6. Airstream patterns during abnormal openings, where slider drag is being cancelled out

The collision of opposite flows depicted in figure 6 should be a rare event - The modern parafoils of today are such that other types of flows between canopy and slider are much likely to occur during normal (i.e. soft ) openings, depending on canopy design specifics: Scenario #1: The dead air scenario of figure 5, in which no flow occurs see figure 7

Canopy bottom skin & stabilizer Air entering cells Air pushing slider upwards No air flowing in between bottom skin and slider top; being instead deflected outwards Figure 7. Airstream patterns during normal openings, Scenario #1 dead-air scenario (see also figure 5)

Why is SDC a rare event? Cont d Scenario #2: Front-to-rear, one-directional flow figure 8 (next slide). >The bottom skin of the wing is not horizontal but inclined >This incline is what gives a wing a good glide during flight; without it the canopy would surge back-and-forth, falling like a leaf >During openings that generate air motion between the slider and bottom skin (or through-flow), the incline promotes this flow to occur in one direction only, i.e. from front to rear >Because the through-flow is perpendicular to the overall relative wind stricking the slider under-surface, the pressure above the slider is lower above its surface than under (remember Bernouilli s principle) - thus leading to non-zero slider drag

Air entering cells Air entering the front gap and exiting through the rear gap facilitated by the incline of bottom skin; yields a lower pressure there Airstream being deflected rearward by through-flow Air pushing slider upwards Side view of canopy Figure 8. Scenario #2: Airstream patterns between the canopy bottom skin and slider during normal openings

Bottom line: slider drag should exist when the air between canopy bottom skin is either dead or through-flowing from front to rear.

Note that the incline could also promote a high pressure area above the slider (and therefore SDC), in the event that the through-flow is mainly rear-to-front

Why should SDC occur at all? - The inflation dynamics of a ram-air wing is quite sensitive on the manner the canopy unfolds right after extraction from the deployment bag - Such unfolding is to some extent random, given the randomness associated with how the canopy and slider are folded inside the deployment bag - Unfolding randomness may also be exacerbated by the turbulence embedded in the airstream hitting the unfolding canopy (including turbulence created by the jumper, btwy) - and also by canopy surging motions that may occur right after bag-extraction - Flow-through between bottom skin and slider is likely to be initiated or suppressed by such random initial conditions

3. How to reduce the occurrence of SDC?

How to reduce the lieklyhood of SDC? Try to eliminate any possibilty for colliding throughflows between the canopy bottom skin and slider surface Theoretically, one way of doing this could be to use domed sliders (figure 9 next slide): - They inflate very quickly, i.e. before through-flows above the slider could have been established - By having fullness, inflated domed sliders would effectively block adverse through-flows from taking place

Canopy bottom skin & stabilizer (black); and domed slider inside, between stabilizers (red) Only airflow: into cells Figure 9. How a domed slider could block adverse through-flow

4. Concluding remarks

- At the moment SDC is a hypothesis which sounds plausible but is in desparate need of experimental evidence - A tip for SDC could be the occurrence of a totally spread-out, but uninflated canopy, captured on video as a jumper looks up at the end of opening - Note again that SDC can exhert its negative effects on its own, or in tandem with slider rebound, or with other negative dynamics that provoke hard openings.

Please send all questions to: potvinj@slu.edu or peek@industrologic.com