AE-705 Introduction to Flight Capsule-05 Lecture-10
Drag And Its Reduction Siddharth Joshi Mechanical Engg. Deptt. VIT - - PowerPoint PPT Presentation
Drag And Its Reduction Siddharth Joshi Mechanical Engg. Deptt. VIT - - PowerPoint PPT Presentation
AE-705: Introduction to Flight Drag And Its Reduction Siddharth Joshi Mechanical Engg. Deptt. VIT Vellore AE-705 Introduction to Flight Lecture-10 Capsule-05 Source: https://upload.wikimedia.org/wikipedia/commons/4/4a/George_Cayley2.jpg SIR
AE-705 Introduction to Flight Capsule-05 Lecture-10
INTRODUCTION TO DRAG
Source: https://upload.wikimedia.org/wikipedia/commons/4/4a/George_Cayley2.jpg
SIR GEORGE CAYLEY (1773 – 1857)
AE-705 Introduction to Flight Capsule-05 Lecture-10
DRAG
Force opposing motion of Aircraft Drag generated due to ΔV
ΔV= Vsolidobject - Vfluid
If ΔV=0 ↔ No motion between solid and fluid ↔ No Drag
Source: https://s-media-cache-ak0.pinimg.com/originals/51/42/b3/5142b32c3fedf745c39ce11aa16be27d.gif
AE-705 Introduction to Flight Capsule-05 Lecture-10
Thrust Drag Airflow
Source: https://encrypted-tbn0.gstatic.com/images?q=tbn:ANd9GcQO0LNN_VHhty3cDXpBKBa3Nd4FTA55BsbpLdfa8pVO3Dxo1ghz
Drag // direction of the free-stream velocity of the airflow
AE-705 Introduction to Flight Capsule-05 Lecture-10
Thrust > Drag
Source: https://tenor.com/view/batman-airplane-gif-5249888 Source: http://www.dccomics.com/sites/default/files/video/THE_LEGO_BATMAN_MOVIE_TRAILER_2_thumb_56f9a68c4f62a0.07314395.jpgDrag must be overcome by Thrust in order to achieve forward motion
AE-705 Introduction to Flight Capsule-05 Lecture-10
Source: https://i1.wp.com/cdn.makezine.com/uploads/2014/01/aeronautics.png
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
But who was the first person to
- bserve
Drag?
George Cayley [1773-1857]
Father of Aviation Identified the four forces- Weight Lift Drag Thrust
AE-705 Introduction to Flight Capsule-05 Lecture-10
Cayley’s Whirling Arm Apparatus
AE-705 Introduction to Flight Capsule-05 Lecture-10
Cayley’s Boy Carrier, 1849
- J. A. D. Ackroyd, Sir George Cayley: The Invention of the Aeroplane near Scarborough at the Time of Trafalgar,
Journal of Aeronautical History Paper No. 2011/ 6130
AE-705 Introduction to Flight Capsule-05 Lecture-10
Cayley’s Governable Parachute, 1852
Original Drawing 1852 Full Scale Replica 1974
AE-705 Introduction to Flight Capsule-05 Lecture-10
Please, Sir George, I wish to give notice, I
was hired to drive and not to fly !
The Reluctant Airman
John Appleby
- Cayley’s Coachman
First manned flight
- n an HTA aircraft
~ 153 m Brompton-by-
Sawdon, near Scarborough, UK
Scene from Anglia TV Ltd, series "On The Wing“, 1974
AE-705 Introduction to Flight Capsule-05 Lecture-10
Full Scale replica flown by Derek Piggot in 1972
AE-705 Introduction to Flight Capsule-05 Lecture-10
Sir George Cayley : Summing Up
AE-705 Introduction to Flight Capsule-05 Lecture-10
COMPONENTS OF DRAG
Breaking Drag down to bits and pieces !
AE-705 Introduction to Flight Capsule-05 Lecture-10
Drag= Profile Drag + Induced Dag + Wave Drag
Pressure Drag + Skin Friction Drag
Also called Form Drag Laminar or Turbulent
Profile Drag independent
- f lift
Also called Parasite Drag
Additional Profile Drag due to lift
Should be small at cruise
Due to lift generated vorticity shed into wake
Supersonic
Drag due to generation of shock waves
Wave drag due to lift Wave drag due to volume
Drag due to lift Zero lift Drag Zero lift Drag
Subsonic
AE-705 Introduction to Flight Capsule-05 Lecture-10
INDUCED DRAG
Source: http://howthingsfly.si.edu/sites/default/files/image-large/il_wingtipvortexedit_lg.jpg
AE-705 Introduction to Flight Capsule-05 Lecture-10
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Lets see how Induced Drag is generated
AE-705 Introduction to Flight Capsule-05 Lecture-10
Source: http://cdn-image.travelandleisure.com/sites/default/files/styles/1600x1000/public/delta0315-party-plane.jpg?itok=BgvL7aanTotal Force Vertical component → Lift Total Force Horizontal Component → Induced Drag
Relative Wind Total Force Induced Drag Weight Lift Thrust
Total aerodynamic force generated by the wing is tilted backwards
AE-705 Introduction to Flight Capsule-05 Lecture-10
Drag created due to the vortices at the tip of the aircraft's wing
Source: https://upload.wikimedia.org/wikipedia/commons/6/68/US_Navy_110606-N-DR144-314_An_F-A-18E_Super_Hornet_assigned_to_Strike_Fighter_Squadron_%28VFA%29_81_maneuvers_over_the_Nimitz-class_aircraft_carrier_US.jpgAirflow at the tips of the wings to curl around in a circular motion
AE-705 Introduction to Flight Capsule-05 Lecture-10
EXPRESSION FOR INDUCED DRAG
Di = 1 2 ρ0Ve
2SCDi
Source: https://upload.wikimedia.org/wikipedia/en/3/39/Induce_drag_downwash.png
CDi = kCL
2
π𝐁𝐒 CL = L 1 2 ρ0Ve
2S
Di = kL2 1 2 ρ0Ve
2Sπ𝐁𝐒 Aspect Ratio Wing Area Lift Air Density Equivalent Airspeed
&
Induced Drag
AE-705 Introduction to Flight Capsule-05 Lecture-10
FACTORS AFFECTING INDUCED DRAG
- 1. Angle of Attack
- 2. Airspeed
- 3. Aspect Ratio
Source: http://aeroscholars.com/multimedia/img/airspeed_indicator.gif
Source: http://www.pilotwings.org/uploads/2/1/9/3/21932436/8536864.jpg?461α
Relative Wind →
Low Aspect Ratio wings High Aspect Ratio wings
Source: https://www.skybrary.aero/images/thumb/AoA.jpg/400px-AoA.jpg
NEXT
AE-705 Introduction to Flight Capsule-05 Lecture-10
Lift ↑ ↔ Induced Drag ↑ ↔ Angle of Attack ↑ Lift and Induced drag ↑ with Angle of Attack upto the critical angle (stall takes place) BACK
Source: http://studysoaring.stlsoar.org/clvsaoa.gif
AE-705 Introduction to Flight Capsule-05 Lecture-10
CL ↑ ↔ Induced Drag ↑ ↔ Airspeed ↓ Low speed ↔ Angle of Attack ↑ ↔ Drag ↑ High speed ↔ Angle of Attack ↓ ↔ Drag ↓
Di = kL2 1 2 ρ0Ve
2Sπ𝐁𝐒
Source: http://www.pilotwings.org/uploads/2/1/9/3/21932436/1042520.jpg?426
Di ↔ 1 Ve
2
BACK
AE-705 Introduction to Flight Capsule-05 Lecture-10
Induced Drag ↑ ↔ Aspect Ratio ↓ Aspect Ratio ↑ ↔ Thinner Wing ↔ Smaller wing vortices ↔ Induced Drag ↓
Source: https://www.youtube.com/watch?v=JMjUxn2cqSI
BACK
AE-705 Introduction to Flight Capsule-05 Lecture-10
Increasing Aspect Ratio
Longer span wing ↔ higher aspect ratio ↔ less induced drag
Boeing B-52
Limitation: Thin long wing requires a large structural weight to support it
Source: http://www.aerospaceweb.org/aircraft/bomber/b52/b52_21.jpg Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Lets see a High Aspect Ratio RC Plane
AE-705 Introduction to Flight Capsule-05 Lecture-10
Tip Plates Inhibit the formation of tip vortices
Source: https://upload.wikimedia.org/wikipedia/commons/thumb/e/e0/Grob_G103C_Glider.jpg/1280px-Grob_G103C_Glider.jpg
Source: http://www.derbyaeroclub.com/Pictures/bory.JPG
AE-705 Introduction to Flight Capsule-05 Lecture-10
Winglets
Reduces the strength of wingtip vortices
Source: http://www.pilotwings.org/uploads/2/1/9/3/21932436/5770030.jpg?334
Converts some of the otherwise-wasted energy in the wingtip vortex to thrust
Source: https://upload.wikimedia.org/wikipedia/commons/thumb/5/5a/Winglet_B737-800.JPG/220px-Winglet_B737-800.JPG Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Lets see how Winglets work
AE-705 Introduction to Flight Capsule-05 Lecture-10
Wing Grid
Source: http://www.reaa.ru/yabbfiles/Attachments/1041849_003.jpg
- 60% ↓ Dinduced compared to
conventional wings
- Increased resistance to tip stall
- Increased overall lift
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
But why are Wing Grids used?
Source: http://www.allstar.fiu.edu/aero/images/Uhuseitehinten175.jpg
Source: http://www.allstar.fiu.edu/aero/winggrid2.htmlAE-705 Introduction to Flight Capsule-05 Lecture-10
Spiroids
Eliminate concentrated wingtip vortices
Source: https://upload.wikimedia.org/wikipedia/commons/b/b2/Spiroid_winglet.jpg
Source: http://airpigz.com/blog/2010/8/27/poll-spiroids-funky-circular-winglets-love-em-or-hate-em.htmlAE-705 Introduction to Flight Capsule-05 Lecture-10
REDUCING PARASITE DRAG
Source: https://www.youtube.com/watch?v=WTTKFqm20RY
AE-705 Introduction to Flight Capsule-05 Lecture-10
PARASITE DRAG
Produced by objects that disrupt the air flow PARASITE DRAG
Form Drag Skin Friction Drag Interference Drag
Source: http://www.pilotwings.org/uploads/2/1/9/3/21932436/1563066.jpg?341Source: http://aeronotes.weebly.com/uploads/2/5/3/7/25370889/7808429.gif?368
Source: http://www.boldmethod.com/images/learn-to-fly/aerodynamics/parasite-drag-and-your-airplane/skin-friction-drag.jpgAE-705 Introduction to Flight Capsule-05 Lecture-10
Parasite Drag ↑ ↔ Airspeed ↑
Source: http://www.pilotwings.org/uploads/2/1/9/3/21932436/5904046.jpg?443
At high speeds ↔ Parasitic Drag > Induced Drag At Low speeds ↔ Induced Drag > Parasite Drag
AE-705 Introduction to Flight Capsule-05 Lecture-10
FORM DRAG
Created by objects deflecting and disrupting air flow
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Objects such as?
Source: https://s-media-cache-ak0.pinimg.com/originals/f1/8f/e4/f18fe4647d0b58e3df0fa7f5b3ee175c.jpg
Landing Gear
AE-705 Introduction to Flight Capsule-05 Lecture-10
FORM DRAG
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Objects such as?
Source: https://i.stack.imgur.com/3KB80.jpg
Antenna
AE-705 Introduction to Flight Capsule-05 Lecture-10
FORM DRAG
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Objects such as?
Source: https://upload.wikimedia.org/wikipedia/commons/thumb/2/26/Wing_Brace_strut.JPG/1280px-Wing_Brace_strut.JPGWing Struts
AE-705 Introduction to Flight Capsule-05 Lecture-10
FORM DRAG
Laminar flow
Source: http://www.pilotwings.org/uploads/2/1/9/3/21932436/5565432.jpg?264
Disruption by Object
Turbulent Flow
Air
AE-705 Introduction to Flight Capsule-05 Lecture-10
Application: Spoilers → Helps the plane to slow down
FORM DRAG
AE-705 Introduction to Flight Capsule-05 Lecture-10
FORM DRAG
Cross sectional Area ↑ ↔ Form Drag ↑
Boeing 747 F-16 Cessna 172
Form Drag decreases
AE-705 Introduction to Flight Capsule-05 Lecture-10
SKIN FRICTION DRAG
Created by the movement of air flow near the skin of the aircraft
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
But what causes skin friction drag?
AE-705 Introduction to Flight Capsule-05 Lecture-10
SKIN FRICTION DRAG
𝐃𝐠 = 𝛖𝐱 𝐫
Skin friction coefficient Cf
Shear stress Dynamic pressure
Cf varies with
- Reynolds number
- Mach number
- Character of the boundary layer
AE-705 Introduction to Flight Capsule-05 Lecture-10
INTERFERENCE DRAG
Generated by mixing of airflow streamlines between airframe components
Source: http://learntoflyblog.com/wp-content/uploads/2016/04/4-6-768x575.png
Wing and Fuselage intersection
AE-705 Introduction to Flight Capsule-05 Lecture-10
Intersection of airstreams creates eddy currents and turbulence
INTERFERENCE DRAG
AE-705 Introduction to Flight Capsule-05 Lecture-10
INTERFERENCE DRAG
Smaller Angle ↔ Interference Drag ↑
Source: http://www.boldmethod.com/images/learn-to-fly/aerodynamics/how-interference-drag-affects-your-airplane-performance/angles-interference-drag.jpgAE-705 Introduction to Flight Capsule-05 Lecture-10
Reduction of Parasite Drag
Streamlining
Contouring of the aircraft’s body to reduce drag
Source: http://www.flyingmag.com/sites/flyingmag.com/files/styles/medium_1x_/public/import/2014/sites/all/files/_images/201404/Lancair-gear.jpg?itok=UfG_seJuLancair Evolution Landing Gear
AE-705 Introduction to Flight Capsule-05 Lecture-10
Reduction of Parasite Drag
Streamlining
Contouring of the aircraft’s body to reduce drag
Source: http://mthobby.pcperfect.com/ch601/Cowling_model.bmp
CH601 Cowling
AE-705 Introduction to Flight Capsule-05 Lecture-10
Reduction of Parasite Drag
Streamlining
Contouring of the aircraft’s body to reduce drag
Source: http://www.zenithair.com/zodiac/607/ph-zen.jpg
Zodiac XL Tail Dragger
AE-705 Introduction to Flight Capsule-05 Lecture-10
Reduction of Parasite Drag
Streamlining
Contouring of the aircraft’s body to reduce drag
Source: https://i.stack.imgur.com/HtsVp.jpg
Boeing 787 Engine Nacelle
AE-705 Introduction to Flight Capsule-05 Lecture-10
Fairings
Act as covers for gaps and spaces between parts of an aircraft to reduce interference drag
Source: http://www.boldmethod.com/images/learn-to-fly/aerodynamics/how-interference-drag-affects-your-airplane-performance/fairings-wing.jpgAE-705 Introduction to Flight Capsule-05 Lecture-10
Fairings
Act as covers for gaps and spaces between parts of an aircraft to reduce interference drag
Source: http://www.zenithair.com/zodiac/607/601-ul-td.jpg
Landing Gear Fairings
AE-705 Introduction to Flight Capsule-05 Lecture-10
Fairings
Act as covers for gaps and spaces between parts of an aircraft to reduce interference drag
Source: https://upload.wikimedia.org/wikipedia/commons/8/87/Ba_b757-200_g-bpei_closeup_arp.jpg
Boeing 757 Flap Track Farings
AE-705 Introduction to Flight Capsule-05 Lecture-10
Tail Cones
Source: http://www.cap-ny153.org/Fairing%20Tail%20Cone.jpg
Reduces the form drag of the fuselage
Source: http://www.cap-ny153.org/Fairing%20Tail%20Cone%202.jpg
AE-705 Introduction to Flight Capsule-05 Lecture-10
Tail Cones
Source: http://www.cap-ny153.org/Fairing%20Tail%20Cone.jpg
Reduces the form drag of the fuselage
Source: http://www.cap-ny153.org/Fairing%20Tail%20Cone%202.jpg
AE-705 Introduction to Flight Capsule-05 Lecture-10
Smart Vortex Generator (SVG)
Devices to delay or prevent flow separation SVGs change their shape autonomously Take off → vortex-generating position During Flight → drag reduction position
Source: https://image.slidesharecdn.com/windpowerengineering-vortexgeneratorsonwindturbineswebinar-151005235800-lva1-app6891/95/windpower-engineering-webinar-vortex-generators-on-wind-turbines-8-638.jpg?cb=1444089612Vortex Generators
AE-705 Introduction to Flight Capsule-05 Lecture-10
Joint Wings
Source: http://aero.stanford.edu/reports/nonplanarwings/JWConcept.jpg
Thinner, smaller chord and higher aspect ratio wings
AE-705 Introduction to Flight Capsule-05 Lecture-10
Strut Braced Wings
Source: https://www.researchgate.net/profile/Eli_Livne/publication/256186912/figure/fig20/AS:392583424561154@1470610590070/Figure-44-Key-elements-of-the-2011-Strut-Braced-Wing-concept-UAV.jpgBadly designed struts can cause massive interference Significant reductions in both vortex and wave drag
AE-705 Introduction to Flight Capsule-05 Lecture-10
Blended Wing Concept Reduction of boundary layer separation regions
Blended Wing Body (BWB) Aircraft
Source: http://i.dailymail.co.uk/i/pix/2016/09/12/16/383F15A900000578-3785673-image-m-2_1473694784931.jpg
AE-705 Introduction to Flight Capsule-05 Lecture-10
WAVE DRAG
Source: https://media.tenor.com/images/a14b376bb5e882cb6db2d32aaa45e272/tenor.gif
AE-705 Introduction to Flight Capsule-05 Lecture-10
Wave Drag
Drag generated by shock waves Occurs at transonic and supersonic speeds
Shock Wave Airflow separation causing wave drag
Source: http://www.boldmethod.com/images/learn-to-fly/aerodynamics/wing-sweep/wave-drag.jpg Source: http://bestanimations.com/Military/Planes/jet-fighter-military-plane-animated-gif-4.gif
AE-705 Introduction to Flight Capsule-05 Lecture-10
Wave Drag Reduction
Swept Wings Backward/Forward angled wings Delays Shock waves and reduces drag
Source: http://www.military-today.com/aircraft/tupolev_tu160_blackjack.jpg
Tupolev Tu-160
Source: http://cdn.toonvectors.com/images/35/122772/toonvectors-122772-940.jpg
Here’s a Swept wing in action
AE-705 Introduction to Flight Capsule-05 Lecture-10
Küchemann Carrots
Source: http://i1285.photobucket.com/albums/a585/hotelalpha200/1040796_zpsgb5ev0vu.jpg
Anti shock body → reduces wave drag at transonic speeds
Convair 990 Coronado
AE-705 Introduction to Flight Capsule-05 Lecture-10