CEA5F0CC-AEE0-4568-8027-F49473406AAE

MODULE b6 : TRANSONIL AERODDMNAMICS Qq.os. Za /1 ¥ Wind Seck Wove — ‘h:,oc& SHUUUWA - formedd on otm.a-rw:rg N Suee SPARAS ¥ Creoied due to Comprestion of € resMs In suddlen worease in M,Wmaw NOIES Bow Setione = svhockioves that forrnm of ARonT or LE oF AC movng ot SUPERSENIC SPCEDS oA, p g ED\O $HWA\E Crovocitrised ay SWAARN & NINSR INCrEGSR. ' Qir P essue, " Compression ofF air n front of AC raisRS temperature - W&duxwvj QNG MO a1 < 1NAAAL =¥ _Resutr froon Mw%a‘r ose fOster Hhan %(mhrfi ' _Bneggmm of waves anead is Ser than normal rade Seck. Gt resemiciing e Srope - utj wordds lnereased \ol SOS T Exends oneod to Eoint of novmal emperature \. Supersonc foe A, Sl frnohion . Sonk ‘oo At Ma \.0 - the waves will form swckinove well aneodd — ‘60\» wave" Ar M_ >0 == AC COfTheS up & \ow WONE affacngs o LE TS entouroge paxess =2 shovie LE s wseol Ccnwesflm@&*%) I\ WAVES " €orm Olove Ma D.8S *M‘mgsmd Rls\er%hannu . Thinner agwofoll a. Lescamb«ad.wng 3. Sweeplonck \T Inreose AOA = accierate \oco\ arflow over wing) SWOCKIWOVRS form af lower Ma A ose of shottwave 0 BGL (xww.g \oyer) = Row remains Suosonic Preseue distuicon(eS flom ernirdl sotlwave \el Gk n &L Thickening oF \ayer forms an celique SecrVave MeroR wl moin snocave (ameda foor = 1) M . _OF ghotrwoNes foron daperols | [. Berofoil Shage > Thickness [ nord vaho =2 Cameer Lambda (L) foot \ / Normal shockwave Subsonic flow Supersonic flow Subsonic flow Subsonic fiow Supersonic flow <+—— Normal shockwave