EXPERIMENTAL DETERMINATION OF 3-DIMENSIONAL LIQUID ROCKET NOZZLE ADMITTANCES

被引:16
作者
ZINN, BT [1 ]
BELL, WA [1 ]
DANIEL, BR [1 ]
SMITH, AJ [1 ]
机构
[1] GEORGIA INST TECHNOL,ATLANTA,GA 30332
关键词
D O I
10.2514/3.6741
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:267 / 272
页数:6
相关论文
共 16 条
[1]  
Bell W. A., 1972, THESIS GEORGIA I TEC
[2]  
BUFFUM FG, 1966, 3932 NAV ORDN TEST S
[3]   VERIFICATION OF NOZZLE ADMITTANCE THEORY BY DIRECT MEASUREMENT OF THE ADMITTANCE PARAMETER [J].
CROCCO, L ;
MONTI, R ;
GREY, J .
ARS JOURNAL, 1961, 31 (06) :771-775
[4]  
CROCCO L, 1965, 10 S INT COMB, P1101, DOI DOI 10.1016/S0082-0784(65)80249-1
[5]  
CROCCO L, 1956, AGARD8
[6]  
CROCCO L, 1967, AGARD117
[7]   ANALYSIS OF ACOUSTIC WAVES IN A COLD-FLOW ROCKET [J].
CULICK, FEC ;
DEHORITY, GL .
JOURNAL OF SPACECRAFT AND ROCKETS, 1969, 6 (05) :591-&
[8]  
GATELY WS, 1969, J ACOUSTICAL SOCIETY, V46, P6
[9]  
LIPPERT WKR, 1953, ACUSTICA, V3, P153
[10]   AN ALGORITHM FOR LEAST-SQUARES ESTIMATION OF NONLINEAR PARAMETERS [J].
MARQUARDT, DW .
JOURNAL OF THE SOCIETY FOR INDUSTRIAL AND APPLIED MATHEMATICS, 1963, 11 (02) :431-441