TIME-DEPENDENT CALCULATIONS FOR TRANSONIC NOZZLE FLOW

被引:10
作者
MIGDAL, D
KLEIN, K
MORETTI, G
机构
[1] Grumman Aircraft Engineering Corporation, Propulsion Project Enginee, Bethpage, NY
[2] Grumman Aircraft Engineering Corporation, The Polytechnic Institute of Brooklyn, Bethpage, NY
关键词
D O I
10.2514/3.5114
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:372 / &
相关论文
共 13 条
[1]   COMPARISON OF MEASURED AND PREDICTED FLOWS THROUGH CONICAL SUPERSONIC NOZZLES WITH EMPHASIS ON TRANSONIC REGION [J].
BACK, LH ;
MASSIER, PF ;
GIER, HL .
AIAA JOURNAL, 1965, 3 (09) :1606-&
[2]  
BOHACHEVSKI IO, 1965, 6524 AIAA PAP I
[3]  
BURSTEIN SZ, 1963, NYO10422 AT EN COMM
[4]  
BURSTEIN SZ, 1963, TID4500 RES DEV REP
[5]  
COURANT R, 1956, NYO7689 AT EN COMM R
[6]  
Godunov S.K., 1959, MAT SB, V47, P271
[7]  
KLEIN K, 1968, FSRADI03681 GRUM AIR
[9]  
LAX PD, 1962, NYO9759 AT EN COMM R
[10]  
LAX PD, 1962, TID4500 RES DEV REP