A THEORY OF THE FLOW PAST A SLENDER DELTA WING WITH LEADING EDGE SEPARATION

被引：60

作者：

MANGLER, KW

SMITH, JHB

机构：

来源：

PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES | 1959年 / 251卷 / 1265期

关键词：

D O I：

10.1098/rspa.1959.0102

中图分类号：

O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];

学科分类号：

07 ; 0710 ; 09 ;

摘要：

引用

页码：200 / 217

页数：18

共 20 条

[1] LEADING-EDGE SEPARATION FROM DELTA-WINGS AT SUPERSONIC SPEEDS
ADAMS, MC
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (06): : 430 - 430
[2] Anton L., 1939, ING ARCH, V10, P411
[3] EFFECT OF LEADING-EDGE SEPARATION ON THE LIFT OF A DELTA-WING
BROWN, CE
MICHAEL, WH
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (10): : 690 - &
[4] FINK PT, 1955, 17854 AER RES COUNC
[5] Jones RT, 1946, 835 NAT ADV COMM AER
[6] Kaden H., 1931, ING ARCH, V2, P140, DOI 10.1007/BF02079924
[7] KUCHENMANN D, 1955, UNPUB NONLINEAR LIFT
[8] LAMPERT S, 1954, 2082 CAL I TECH JET
[9] LEGENDRE R, 1952, 30 RECH AER
[10] LEGENDRE R, 1953, 31 RECH AER