SMALL PERTURBATION EXPANSIONS IN UNSTEADY AEROFOIL THEORY

被引:9
作者
GRAHAM, JMR [1 ]
KULLAR, I [1 ]
机构
[1] UNIV LONDON,IMPERIAL COLL SCI & TECHNOL,DEPT AERONAUT,LONDON SW7 2AZ,ENGLAND
关键词
D O I
10.1017/S0022112077001165
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
引用
收藏
页码:209 / 224
页数:16
相关论文
共 22 条
[1]  
ADAMCZYK JJ, 1974, NASA2395 CONTR
[2]  
ADAMCZYK JJ, 1971, THESIS U CONNECTICUT
[3]   AIRFOIL RESPONSE TO AN INCOMPRESSIBLE SKEWED GUST OF SMALL SPANWISE WAVE-NUMBER [J].
AMIET, RK .
AIAA JOURNAL, 1976, 14 (04) :541-542
[4]   LOW-FREQUENCY APPROXIMATIONS IN UNSTEADY SMALL PERTURBATION SUBSONIC FLOWS [J].
AMIET, RK .
JOURNAL OF FLUID MECHANICS, 1976, 75 (JUN11) :545-552
[5]   ACOUSTIC RADIATION FROM AN AIRFOIL IN A TURBULENT STREAM [J].
AMIET, RK .
JOURNAL OF SOUND AND VIBRATION, 1975, 41 (04) :407-420
[6]   COMPRESSIBILITY EFFECTS IN UNSTEADY THIN-AIRFOIL THEORY [J].
AMIET, RK .
AIAA JOURNAL, 1974, 12 (02) :252-255
[7]  
Bisplinghoff R.L., 1996, AEROELASTICITY
[8]  
FILOTAS LT, 1969, NASA SP207, P231
[9]   LIFTING SURFACE THEORY FOR PROBLEM OF AN ARBITRARILY YAWED SINUSOIDAL GUST INCIDENT ON A THIN AEROFOIL IN INCOMPRESSIBLE FLOW [J].
GRAHAM, JMR .
AERONAUTICAL QUARTERLY, 1970, 21 :182-&
[10]   SIMILARITY RULES FOR THIN AEROFOILS IN NON-STATIONARY SUBSONIC FLOWS [J].
GRAHAM, JMR .
JOURNAL OF FLUID MECHANICS, 1970, 43 :753-&