LIFT EFFECTIVENESS OF SLENDER WINGS ON CYLINDRICAL BODIES

被引：5

作者：

MIRELS, H

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1953年 / 20卷 / 07期

关键词：

D O I：

10.2514/8.2702

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：504 / 505

页数：2

共 50 条

[1] LIFT EFFECTIVENESS OF SLENDER WINGS WITH STREAMWISE ROOT GAPS AND FENCES
JUDD, M
[J]. AIAA JOURNAL, 1969, 7 (11) : 2179 - &
[2] MAXIMUM LIFT ON SLENDER WINGS
BRIDSON, DW
[J]. AERONAUTICAL JOURNAL, 1970, 74 (716): : 671 - &
[3] LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
MESSITER, AF
[J]. AIAA JOURNAL, 1963, 1 (04) : 794 - 802
[4] ON LIFT OF VERY SLENDER-WINGS AT LOW SPEED
EHRLICH, E
DESIEVER.A
[J]. RECHERCHE AEROSPATIALE, 1967, (121): : 29 - &
[5] HIGH-FREQUENCY OSCILLATION OF SLENDER BODIES AND WINGS
HANIN, M
[J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (07): : 544 - 545
[6] SIMILARITY IN VORTEX ASYMMETRIES OVER SLENDER BODIES AND WINGS
KEENER, ER
CHAPMAN, GT
[J]. AIAA JOURNAL, 1977, 15 (09) : 1370 - 1372
[7] THE WAVE DRAG AT ZERO LIFT OF SLENDER DELTA WINGS AND SIMILAR CONFIGURATIONS
LIGHTHILL, MJ
[J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (03) : 337 - 348
[8] PRESSURE DISTRIBUTION ON SLENDER BODIES AND WINGS OSCILLATING AT HIGH FREQUENCY
HANIN, M
[J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (11): : 905 - 906
[9] LIFT-TO-DRAG RATIOS OF SLENDER BODIES AT HYPERSONIC SPEEDS
MIELE, A
[J]. JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1966, 13 (01): : 1 - &
[10] EXPERIMENTAL STUDY OF VERY LOW ASPECT RATIO WINGS IN SLENDER BODIES
Arevalo-Campillos, M. A.
Tuling, S.
Parras, L.
del Pino, C.
Dala, L.
[J]. PROCEEDINGS OF THE ASME 11TH BIENNIAL CONFERENCE ON ENGINEERING SYSTEMS DESIGN AND ANALYSIS, 2012, VOL 2, 2012, : 73 - 82