The Effect of Laminar Nozzle Exit Boundary Layer Thickness on a Mach 1.3 Jet With and Without Control
42nd AIAA Fluid Dynamics Conference and Exhibit
2012-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2012
|Effect of Nozzle-Exit Boundary Layer on Jet Noise
AIAA | 2013
|Effect of Nozzle-Exit Boundary Layer on Jet Noise
British Library Conference Proceedings | 2013
|