The use of energy thickness in prediction of throat heat transfer in rocket nozzles
1969
II, 29 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
ROCKET NOZZLE MODELLING - Throat Flow Modelling of Expansion Deflection Nozzles
Online Contents | 2004
|Analysis of heat transfer in rocket nozzles
AIAA | 1996
|Analysis of Heat Transfer in Rocket Nozzles
British Library Conference Proceedings | 1996
|