Question

M

Consider a 2D inviscid flow supersonic wind tunnel as in Fig. 1.4

Nozzle

Mtest

Test section

Fig. 1 Wind Tunnel

Mexit

L

Design a wind tunnel nozzle that maintains uniform supersonic flow in the test section at a

Mach number of 3.0, given an inflow Mach number of 0.3. Provide a detailed explanation of

the designed geometry, including the contour results.

Question image 1