LIFT AND MOMENT FOR ARBITRARY POWER-LAW UPWASH IN OSCILLATING SUBSONIC UNSTEADY THIN-AIRFOIL THEORY

被引:4
作者
KEMP, NH [1 ]
机构
[1] AVCO EVERETT RES LAB INC,EVERETT,MA 02149
关键词
D O I
10.2514/3.49258
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:413 / 415
页数:3
相关论文
共 5 条
[1]   AERODYNAMIC INTERFERENCE BETWEEN MOVING BLADE ROWS [J].
KEMP, NH ;
SEARS, WR .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (09) :585-597
[2]   ON THE LIFT AND CIRCULATION OF AIRFOILS IN SOME UNSTEADY-FLOW PROBLEMS [J].
KEMP, NH .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (10) :713-714
[3]   CLOSED-FORM LIFT AND MOMENT FOR OSBORNES UNSTEADY THIN-AIRFOIL THEORY [J].
KEMP, NH .
AIAA JOURNAL, 1973, 11 (09) :1358-1360
[4]   UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW [J].
OSBORNE, C .
AIAA JOURNAL, 1973, 11 (02) :205-209
[5]  
Sears W. R., 1941, J AERONAUT SCI, V8, P104, DOI [10.2514/8.10655, DOI 10.2514/8.10655]