THE QUARTER-INFINITE WING OSCILLATING AT SUPERSONIC SPEEDS

被引：0

|

作者：

GOODMAN, TR

机构：

来源：

QUARTERLY OF APPLIED MATHEMATICS | 1952年 / 10卷 / 02期

关键词：

D O I：

10.1090/qam/51093

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

引用

收藏

页码：189 / 192

页数：4

相关论文

共 50 条

[31] STEADY-STATE TEMPERATURE DISTRIBUTIONS IN A QUARTER-INFINITE SOLID AND IN A SEMI-INFINITE SOLID INTERNALLY BOUNDED BY A CYLINDER
MANNER, M
CHEMICAL ENGINEERING SCIENCE, 1969, 24 (02) : 267 - &
[32] OBLIQUE WING - AIRCRAFT DESIGN FOR TRANSONIC AND LOW SUPERSONIC SPEEDS
JONES, RT
ACTA ASTRONAUTICA, 1977, 4 (1-2) : 99 - 109
[33] WING-BODY CARRYOVER AT SUPERSONIC SPEEDS WITH FINITE AFTERBODIES
VUKELICH, SR
WILLIAMS, JE
AIAA JOURNAL, 1981, 19 (05) : 661 - 664
[34] AN EXPERIMENTAL ANALYSIS ON EFFECT OF ELASTICITY OF WING ON DOWNWASH AT SUPERSONIC SPEEDS
BUONGIOR.C
AEROTECNICA, 1968, 48 (03): : 56 - &
[35] ON THE LOW ASPECT RATIO OSCILLATING RECTANGULAR WING IN SUPERSONIC FLOW
MILES, JW
AERONAUTICAL QUARTERLY, 1953, 4 (03): : 231 - 244
[36] FLOW OVER A HIGH ASPECT RATIO GOTHIC WING AT SUPERSONIC SPEEDS
NARAYAN, KY
AERONAUTICAL QUARTERLY, 1975, 26 (AUG): : 189 - 201
[37] INTERFERENCE BETWEEN WING AND BODY AT SUPERSONIC SPEEDS - ANALYSIS BY THE METHOD OF CHARACTERISTICS
FERRARI, C
JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (07): : 411 - 434
[38] SOME EXPERIMENTAL RESULTS ON WING-BODY INTERFERENCE AT SUPERSONIC SPEEDS
BAILEY, HE
PHINNEY, RE
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1954, 21 (03): : 285 - 285
[39] COMPUTATIONAL STUDY OF A CONICAL UNIT ASPECT RATIO WING AT SUPERSONIC SPEEDS
MCGRATH, BE
JOURNAL OF AIRCRAFT, 1995, 32 (04): : 877 - 880
[40] INTERFERENCE BETWEEN WING AND BODY AT SUPERSONIC SPEEDS - THEORY AND NUMERICAL APPLICATION
FERRARI, C
JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (06): : 317 - 336

← 1 2 3 4 5 →