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 Stacey Huang   uster http://img453.ima geshack.us/f /58263535yh1.j pg/

Supersonic Airfoils

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7/18/2019 Supersonic Airfoils

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Stacey Huang

   – uster 

http://img453.imageshack.us/f/58263535yh1.jpg/

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Histor of Su ersonic Fli h•   1887: Ernst Mach, shockwaves•   Early 1900’s: NACA research•   1940’s: Multiple attempts to travel 

at supersonic speeds, couldn’t “break the sound barrier” ‒  

 ‒   Compressibility  – shockwaves

•   First supersonic flights:

  http://history.nasa.gov/SP‐4219/4219‐065.jpg

 –   ‐ , •   George Welch on October 1 and October 

14, 1947•   Couldn’t prove how fast the plane was 

 –   Bell X‐1: In level flight, rocket propulsion

•   Charles E. Yeager on October 14, 1947

•   1950 s: W itcom   Area Ru e

http://history.nasa.gov/SP‐4219/4219‐060.jpg

•http://history.nasa.gov/SP‐4219/4219‐083.jpg

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 A General Look At Airfoils

 Any mechanical or organic structure designed for

the purpose of generating lift In airplanes, usually displayed as cross-section, like here ↓

  Leading Edge

Camber (Max, Min) Mean Camber

Chord

Trailin Ed e

Symmetrical

 Asymmetrical (cambered)

http://www.allstar.fiu.edu/aero/flight31.htm

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  http://wings.avkids.

com/Book/Flight/I

mages/airfoil.jpgNewton:Bernoulli:http://virtualskies.arc.nasa.gov/a

eronautics/images/airflow.jpg

Image Cropped From:

http://www.grc.nasa.gov/WWW/K‐12/airplane/Images/newton3.gif 

 

http://hyperphysics.phy‐astr.gsu.edu/Hbase/fluids/imgflu/airfoil.gif 

http://media.photobucket.com/image/newton%252527s%203rd%2

•   ng e 

ttac

 –  Flying 

upside 

down

0law%20airfoil leftieman Aircraft%2520Physics%2520Discussion%2

520Images/airfoil.jpg

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  The Mach Number M (with airplane velocity V 

an 

soun 

ve ocity 

approximate y  *1

given a discrete

 altitude)

 is

 given

 by

 .

  ,  .   Gives an indication for how much faster than 

the s eed

 of 

 sound

 an

 aircraft

 is

 travelin :

 

Mach 2 is twice the speed of  sound.   Critical Mach Number

    pee

 o

 soun :

  1,116.4 ft/s or 761.2 mph 

  .   , .  

  661.5 

knots 

*1 With γ = specific heat ratio; R = specific gas constant;  T = atmospheric temperature

http://www.impactlab.com/wp‐content/uploads/2009/06/3‐43563.jpg

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CHALLENGES IN SUPERSONIC FLIGHT

The "critical speed" at which these occur decreases asthe an le of attack is increased and the airfoil

thickness is increased. Increasingly difficult to maintain lift (lift coefficient

Apparent infinite drag (drag coefficient increases)

Compressibility problems Changes in air density

Flow choking 

Expansion fans

Compressibility burble:uncontrollable dives

Normal shock

Bow shockhttp://history.nasa.gov/SP‐4219/4219‐064.jpg

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http://aero.stanford.edu/Reports/vki_kroo_supersonics.pdf 

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 Conventional

 Canard  Considerations:   Mac   num er: spee   constitutes  esign

  Optimal altitude

  Fuselage: 

higher 

 volume, 

greater 

drag   Optimal area distributions

  Whitcomb 

 Area 

Rule

  Hi h 

overall 

fineness 

ratio

  Low 

boom

  Supersonic Laminar Flow

http://www.compositesworld.com/cdn/cms/HPC0109_beyondtheconcorde_b.jpg

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•  

• SLF (swept wing)

  – ow sweep

 – Pressure gradientshttp://www.aerospaceweb.org/design/psp/figures/fig07.jpg• Oblique

 – Elliptic distributions

http://www.aerospaceweb.org/design/waverider/figures/fig18.jpg

 – Area Rule

 – Structural adv.

http://aero.stanford.edu/Reports/vki_kroo_supersonics.pdf http://www.aviation‐history.com/convair/b58‐3.jpg

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•  Military aircraft

 – Fighter aircraft

•   Stealth aircraft

•   Space shuttle re‐http://www.seorf.ohiou.edu/~af641/sr71001.jpg

•   Business aircraft

http://psipunk.com/wp‐content/uploads/2010/01/supersonic‐business‐ jet‐futuristic‐aircraft‐01.jpg

http://www.nasa.gov/centers/ames/images/content/146600main_sts1anniv‐AC76‐1713.jpg

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Konstantin Eduardovitch Tsiolkovsky

Константин Эдуардович Циолковский

"Men are weak now, and yet they transform 

'   . 

might will increase to the extent that they will 

change the surface of  the Earth, its oceans, the 

atmosphere, and themselves. They will control the climate and the Solar System  just as they 

control the Earth. They will travel beyond the 

limits of  our planetary system; they will reach 

other Suns  and use their fresh ener   instead 

of  the energy of  their dying luminary.”

http://www.informatics.org/museum/tsiol.htmlhttp://www.informatics.org/museum/portoftsiolkovsky.jpg

1857‐

1935Name in Russian script obtained from: http://www.peoples.ru/technics/designer/tsiolkovsky/

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Became deaf at a young age due to illness◦   -

Attended university in Moscow

Then worked as schoolteacher in Kalu a 

Started to publish works about space, butinitially little recognized

After Bolshevik Revolution, he earnedgovernmental support and died famous foris wor

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http://exploration.grc.nasa.gov/education/rocket/Images/rktpow.gif 

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  urther Studies in Rocket lighturther Studies in Rocket light

Rocket ro ellantshttp://www.audacity.org/images/fe

atures/A‐photo‐Apollo‐11/Apollo‐

11‐mission‐launch‐16‐July‐1969.jpg

Liquid propellants: Hydrogen, oxygen Hi h exhaust velocit

Space shuttle designs

Combustion chambers

Pressurized cabins

G rosco es

Etc.

-

http://www.informatic

s.org/museum/graphic

s/rockets.gif 

 

Only way to attain escape velocity into Earth orbit

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http://www.info

rmatics.org/mus

eum/russianscan

%20folder/drawi

 

 

.

 

  Eating, sleeping

 in

 zero

‐gravity

 

  Food and oxygen for colonies

 

  Believed:

’ 

http://www.daviddarling.info/images/Tsiolkovsky_spaceship.jpg

 

  Humans must traverse beyond Earth in order to 

evolve

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Ma or Publications 

Apparatus (1896): space flight“

Machines” (1903): rocket equation

" "

Nauchnoye Obozreniye (Science Review) (1903)

http://www.informatics.org/museum/postcard%20folder/book.jpg

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  “

http://orig.thestarpress.com/blogs/gadgetguy/images/Rocket.jpg

 

human space flight”

  ,

but glorified by USSR

   - pu n

1961 – Yuri Gagarin

http://astroprofsp

age.com/wp‐

content/uploads/

2007/07/Sputnik_

teck.

Influenced work of subsequent scientists

 

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Bibliography: Tsiolkovsky 

“Relativity Calculator – Rocket Equations and Newton’s 3rd Lawof Motion”. elativit Calculator. N.d. Web. 22 Jul 2010.<http://www.relativitycalculator.com/rocket_equations.shtml>

“Rocket Equation”. The Internet Encyclopedia of Science. N.d. Web. 19 Jul 2010.< p: www. av ar ng. n o encyc ope a roc e _equa on.html>

“Tsiolkovsky, Konstantin Eduardovich (1857–1935)”. The. . . . .<http://www.daviddarling.info/encyclopedia/T/Tsiolkovsky.html>

“Tsiolkovsky”. Konstantin E. Tsiolkovsky State Museum of the

 History of Cosmonautics. Informatics International, Inc. N.d. Web. 22 July 2010.<http://www.informatics.org/museum/tsiol.html>“ ”. . . . . . .<http://www.russianspaceweb.com/tsiolkovsky.html>

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http://www.profcardy.com/matematicos/bK

utta.jpg

1867-1944

Mathematician Scientist Historian

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 One 

older 

brother  Parents died when young and brought up by 

an uncle

 Studied Mathematics

 in

 Munich,

 but

 had

 wide range o   interests

 Famous for work in mathematics, aerodynamics, 

glaciers, and

 history

 o

 mathematics

 Later taught as a professor in multiple 

un vers t es aroun   ermany

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-

http://farside.ph.utexas.edu/teac

hing/329/lectures/node35.html

Alternate method of solving differential equations

Used instead of Euler’s method in scientificcomputations

Symmetric integration method (smaller truncation

error Estimation to midpoint to obtain true point

  nt or er requires n eva uations per step

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 Discovered independently 

    crea e    y  a ro a ng cy n er

 Air 

molecules 

entrain 

flow 

in 

http://www‐

mdp.eng.cam.ac.uk/web/library/enginfo/aerotherm

al_dvd_only/aero/fprops/poten/img324.png 

 vortex flow

 Streamlines 

distorted 

from 

L = lift per unit length

ρ = density of  the gas

U∞ = velocit   of  the air

spinning and creates forceΓ = circulation

(strength of  rotation)

http://www‐hm.ma.tum.de/geschichte/kutta2.gif 

http://hyperphysics.phy‐astr.gsu.edu/hbase/fluids/imgflu/kuttajou.gif 

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Miscellaneous Work 

East Alps 

History of mathematics

 

Ellipses

http://www.hickerphoto.com/data/media/152/southern‐alps_17456.jpghttp://cxc.harvard.edu/csc/why/imgs/JD_err_ellipses.jpg

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Bibliography: Kutta

“Kutta Biography”. School of Mathematics and Statistics: University. , . . . .

<http://www-groups.dcs.st-and.ac.uk/~history/Biographies/Kutta.html>

Bulirsch, R., and M. Breitner. “Wilhelm Martin Kutta 1867-1944”.Tec n sc e Un vers t t M nc en, Fa u t t r Mat emat .<http://www-hm.ma.tum.de/geschichte/node21.html> [translated with Google Translate]

  “ - ”Texas at Austin. 29 March 2006. Web. 22 July 2010.<http://farside.ph.utexas.edu/teaching/329/lectures/node35.html>

“ ”

u a- ou ows eorem . yper ys cs. eorg a a eUniversity. N.d. Web. 22 July 2010. <http://hyperphysics.phy-astr.gsu.edu/hbase/fluids/kutta.html>

“Lift of a Rotatin C linder”. NASA. 11 Jul 2008. Web. 2 Jul2010. <http://www.grc.nasa.gov/WWW/K-12/airplane/cyl.html>