Research Article

An Air Jet Distortion Generation System

Table 1

Flow cases chosen for computations.

Sl. numberInlet Mach number, Jet mass flow rate, %Mass flow ratio,
Jet 1Jet 2Jet 3Jet 4

10.175252525250.119
20.186502525250.137
30.214752525250.143
40.2571002525250.141
50.184505050250.184
60.2481002550250.163
7 0.178505050500.210
80.2441002575250.182
90.186755050500.223
100.2201007550250.214
110.25310025100250.193
120.188757550500.240
130.23110050100250.222
140.185757575500.261
150.21710075100250.249
160.178757575750.286
170.212100100100250.268
180.1831007575750.296
190.198100100100500.297
200.182100100100750.329
210.1751001001001000.352