Design of an Intermittent, Single Jack Flexible Nozzle Supersonic Wind-Tunnel for Mach Numbers 1.5 to 4.0
1970
39 pages
Report
Keine Angabe
Englisch
Investigation of a Single-Jack Flexible Supersonic Nozzle AIAA Paper
British Library Conference Proceedings | 2007
|British Library Conference Proceedings | 1992
|Design and Optimisation of a Mach 2.5 Wind Tunnel Nozzle
AIAA | 2023
|