SONIC BOOM WAVEFORMS AND AMPLITUDES IN A REAL ATMOSPHERE

被引:19
作者
GEORGE, AR
PLOTKIN, KJ
机构
关键词
D O I
10.2514/3.5491
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Simple method for determining sonic boom waveshapes and amplitudes in a still stratified atmosphere is presented. The effects of acoustic impedance, ray tube area, and nonlinear wave steepening and shock formation are each treated separately. By restricting consideration to the waves directly below an aircraft in steady flight, it is possible to present all the information needed to calculate wave shapes and amplitudes without use of a computer. The results for the U S Standard Atmosphere are presented and compared to those calculated for various model atmospheres and to the results of various approximations.
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页码:1978 / &
相关论文
共 18 条
[1]  
[Anonymous], 1962, US STANDARD ATMOSPHE
[2]  
GEORGE AR, 1968, SP180 NASA, V2
[3]  
HAYES WD, 1968, SP180 NASA, V2
[4]  
KANE EJ, 1964, AD610643
[5]  
KANE EJ, 1964, RD64160 SRDS REPT FE
[6]  
KAWAMURA R, 1967, 416 U TOK I SPAC AER
[7]  
Landau L. D., 1945, PRIKL MAT MEKH, V9, P286
[8]  
LILLEY GM, 1965, 5 C INT AC, V2, P109
[9]  
LOMAX H, 1958, A55A18 NACA RM
[10]  
MIDDLETON WD, 1968, TND3082 NASA