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Shock Analysis-Advanced Unified Engineering-Assignment Solution, Exercises of Aeronautical Engineering

Jiwaji UniversityAeronautical Engineering

This is solution to assignment of Basic Unified Engineering course. It was submitted to Prof. Yasaar Verma at Jiwaji University. It includes: Shock, Analysis, Flow, Sketch, Oblique, Expansion, Loss, Air, Hose, Bending, Loads

Typology: Exercises

2011/2012

Uploaded on 07/22/2012

senapati_007
senapati_007 🇮🇳

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Download Shock Analysis-Advanced Unified Engineering-Assignment Solution and more Exercises Aeronautical Engineering in PDF only on Docsity!

UE Fluids | Fl/7 + FI Soluhen son by ae eee er Fete == aa oo Shock fe shock ohing be oe g pee a) Oblique Sheek. M= 1,6, O=10° > B= 51° (chart, Anderson p. 513) M,, = M sin Sl? = 1,6°0772 1,243 b./p, = flit, ) = 1.636 (Ardhriom og, 9.16, or Appendic B bbe. ) Sine ps fae a6 R= P| My, A) = wo (os, 7.14) MM, - M, os py = 24S b) Expans/o fur. M) = = M, = |, 2457 , 7/4, ) = 4,7° v(M,) = v(m) + 20" 247° —» M,= |, 94 ne gn ne (not gure te “tet 1 eee, a re He J Lx eth = Gap + hep)§= (-ttips (rasp C= ~ 0,112 I2 poe TL D=D +D, = -L, fan IO” + Ly ton lO" =[- (I- 1,636 + (\-0.598)| tonl0” pS [D's 0. 2 0124 Pol ¢ | Doing 2 A Vp * Spi, = = |. 792 Py >