HOT STREAK CHARACTERIZATION IN SERPENTINE EXHAUST NOZZLES (AIAA 2016-4502)
Joint propulsion conference
01.01.2016
12 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Shape Control of Tensegrity Structures (AIAA 2015-4502)
British Library Conference Proceedings | 2015
|Effect of Geometry on Exit Temperature from Serpentine Exhaust Nozzles (AIAA 2015-1670)
British Library Conference Proceedings | 2015
|DataCite | 1931