Effect of Stagnation Temperature on the Supersonic Axisymmetric Minimum Length Nozzle Conception with Application for Air
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
2009-01-01
Conference paper
Electronic Resource
English
British Library Online Contents | 2007
|Supersonic Two-Dimensional Minimum Length Nozzle Design at High Temperature. Application for Air
British Library Online Contents | 2007
|