Analytical method for including thermodynamic data with variable isentropic exponent in method of characteristics as applied to design of high-temperature rocket exhaust nozzles is obtained; several bell-shaped nozzles are designed and nozzle contours compared showing that significant differences occur; conclusions presented.
Design of axisymmetric exhaust nozzles by method of characteristics incorporating variable isentropic exponent
NASA -- Tech Report
1959
31 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Nonideal isentropic gas flow through converging-diverging nozzles
Tema Archiv | 1990
|