CALCULATION OF PRESSURES ON BODIES AT LOW ANGLES OF ATTACK IN SUPERSONIC-FLOW

被引：4

作者：

DEJARNETTE, FR ^{[1
]}

FORD, CP ^{[1
]}

YOUNG, DE ^{[1
]}

机构：

[1] USN, CTR SURFACE WEAP, AEROMECH BRANCH, DAHLGREN, VA 22448 USA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1980年 / 17卷 / 06期

关键词：

D O I：

10.2514/3.57770

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：529 / 536

页数：8

共 50 条

[1] CALCULATION OF SUPERSONIC-FLOW PAST THE WEATHER SIDE OF A WING OF SMALL ASPECT RATIO AT LARGE ANGLES OF ATTACK
GOLUBKIN, VN
NEGODA, VV
[J]. USSR COMPUTATIONAL MATHEMATICS AND MATHEMATICAL PHYSICS, 1988, 28 (05): : 202 - 208
[2] OPERATIVE CALCULATION OF THE SPATIAL SUPERSONIC-FLOW AROUND BODIES CLOSE TO THE AXISYMMETRICAL BODIES
TIMOSHENKO, VI
GALINSKII, VP
[J]. IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1991, (04): : 22 - 27
[3] OSCILLATING BLUNT BODIES IN SUPERSONIC-FLOW
RUES, D
[J]. ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1974, 22 (07): : 233 - 240
[4] SUPERSONIC-FLOW ABOUT CIRCULAR CONES AT LARGE ANGLES OF ATTACK - FLOATING DISCONTINUITY APPROACH
DAYWITT, J
KUTLER, P
ANDERSON, D
[J]. ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B8 - B8
[5] The optimum airfoils at low angles of attack in a supersonic gas flow
Zubov, VI
[J]. PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS, 1997, 61 (01): : 83 - 91
[6] TRANSONIC SUPERSONIC-FLOW AROUND BODIES OF REVOLUTION
FRANK, W
ZIEREP, J
[J]. ACTA MECHANICA, 1974, 19 (3-4) : 277 - 287
[7] NONLINEAR AERODYNAMIC EFFECTS ON BODIES IN SUPERSONIC-FLOW
PITTMAN, JL
SICLARI, MJ
[J]. JOURNAL OF AIRCRAFT, 1984, 21 (10): : 809 - 815
[8] OSCILLATING WINGS AND BODIES WITH FLEXURE IN SUPERSONIC-FLOW
LIU, DD
GARCIAFOGEDA, P
CHEN, PC
[J]. JOURNAL OF AIRCRAFT, 1988, 25 (06): : 507 - 514
[9] CALCULATION OF HYPERSONIC FLOW OVER BODIES OF REVOLUTION AT SMALL ANGLES OF ATTACK
RAKICH, JV
[J]. AIAA JOURNAL, 1965, 3 (03) : 458 - &
[10] CALCULATION OF SUPERSONIC-FLOW IN CHANNEL OF AN MHD GENERATOR
PONOMAREV, VM
[J]. HIGH TEMPERATURE, 1974, 12 (03) : 533 - 538

← 1 2 3 4 5 →