Nozzle Pressure Ratio Effects on Aerodynamics and Acoustics of a Highly-Heated Rectangular Supersonic Jet
25th AIAA/CEAS Aeroacoustics Conference
2019-01-01
Conference paper
Electronic Resource
English
Theory of aerodynamics of supersonic splitline gimbaled nozzle
Engineering Index Backfile | 1967
|Aerodynamics and acoustics of rectangular and swept rotor blade tips
Tema Archive | 1989
|Rotorcraft Acoustics & Aerodynamics
Online Contents | 1997