DESIGN METHODS FOR MINIMAZATION OF SONIC-BOOM PRESSURE-FIELD DISTURBANCES

被引:4
作者
MCLEAN, FE
SHROUT, BL
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D O I
10.1121/1.1914039
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O42 [声学];
学科分类号
070206 ; 082403 ;
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页码:S19 / &
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共 7 条
[1]   SONIC-BOOM PRESSURE-FIELD ESTIMATION TECHNIQUES [J].
CARLSON, HW ;
MACK, RJ ;
MORRIS, OA .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1966, 39 (5P2) :S10-&
[2]  
Carlson HW., 1964, J AIRCRAFT, V1, P82, DOI [10.2514/3.43562, DOI 10.2514/3.43562]
[3]  
CARLSON HW, 1962, D1494 NASA TECH NOT
[4]   EFFECTS OF ATMOSPHERE AND AIRCRAFT MOTION ON THE LOCATION AND INTENSITY OF A SONIC BOOM [J].
FRIEDMAN, MP ;
KANE, EJ ;
SIGALLA, A .
AIAA JOURNAL, 1963, 1 (06) :1327-1335
[5]  
JONES LB, 1961, ROY AERON SOC TECH N, V65, P433
[6]  
MAGLIERI DJ, 1965, SP83 NASA C AIRCR OP, P245
[7]  
MCLEAN FE, 1965, D2877 NASA TECH NOT