oD An oblique shock Wav nas the following upstream static conditions and Machnumber : P-150 kPa ,T-500 A, M-1.605 and a shock angle ß =60°. It is required to calculate1. Upstream velocity V1 and deflection angle 6.2. Downstream Mach number M23. Static and stagnation temperature (T2, To2)4. Downstream velocity V2.54. Normal and tangential velocity component upstream and downstream of the oblique shock(Vin, Vit, V2n, Va )6 9. Static and stagnation pressure (P2, Pol).

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Q1) An oblique shock wave has the following upstream static conditions and Mach Dumber : P=150 kPa ,T-500 K, Mj=1.605 and a shock angle B =60°. It is required to calculate 1. Upstream velocity V1 and deflection angle A 2. Downstream Mach number M2 3. Static and stagnation temperature (T2, To2) 4. Downstream velocity V2. S4. Normal and tangential velocity component upstream and downstream of the oblique shock (Vin, Vit, V2n , Va) 6 9. Static and stagnation pressure (P2, Pol).

Q1) An oblique shock wave has the following upstream static conditions and Mach Dumber : P=150 kPa ,T-500 K, Mj=1.605 and a shock angle B =60°. It is required to calculate 1. Upstream velocity V1 and deflection angle A 2. Downstream Mach number M2 3. Static and stagnation temperature (T2, To2) 4. Downstream velocity V2. S4. Normal and tangential velocity component upstream and downstream of the oblique shock (Vin, Vit, V2n , Va) 6 9. Static and stagnation pressure (P2, Pol).

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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