HIGH-FREQUENCY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW

被引:119
作者
AMIET, RK [1 ]
机构
[1] UNITED TECHNOL RES CTR,E HARTFORD,CT 06608
关键词
D O I
10.2514/3.7187
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:1076 / 1082
页数:7
相关论文
共 19 条
[1]  
Adamczyk J. J., 1974, Journal of Aircraft, V11, P281, DOI 10.2514/3.59240
[2]   SCATTERING OF SOUND BY AN AEROFOIL OF FINITE SPAN IN A COMPRESSIBLE STREAM [J].
ADAMCZYK, JJ ;
BRAND, RS .
JOURNAL OF SOUND AND VIBRATION, 1972, 25 (01) :139-&
[3]  
ADAMCZYK JJ, AIAA73683 PAP
[4]  
ADAMCZYK JJ, CR2395 NASA
[5]   ACOUSTIC RADIATION FROM AN AIRFOIL IN A TURBULENT STREAM [J].
AMIET, RK .
JOURNAL OF SOUND AND VIBRATION, 1975, 41 (04) :407-420
[6]  
AMIET RK, 1975, MAR P S UNST AER, P631
[7]  
Amiet RK, 1974, AIAA J, V12, P253
[8]   PREDICTION OF UNSTEADY AIRLOADS FOR OBLIQUE BLADE-GUST INTERACTION IN COMPRESSIBLE FLOW [J].
CHU, S ;
WIDNALL, SE .
AIAA JOURNAL, 1974, 12 (09) :1228-1235
[9]  
Drischler J.A, 1956, 3748 NASA TN
[10]   AERODYNAMIC COEFFICIENTS OF AN OSCILLATING AIRFOIL IN 2-DIMENSIONAL SUBSONIC FLOW - COMMENT [J].
FETTIS, HE .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (05) :353-354