INFLUENCE OF A GIVEN CONICAL BODY ON MINIMUM DRAG PROBLEM OF A DELTA WING, IN SUPERSONIC FLOW

被引：0

|

作者：

NASTASE, A

机构：

来源：

RECHERCHE AEROSPATIALE | 1971年 / 02期

关键词：

D O I：

暂无

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：99 / &

相关论文

共 50 条

[1] THE SUPERSONIC CONICAL WING OF MINIMUM DRAG
TSIEN, SH
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (12): : 805 - &
[2] A WING-BODY PROBLEM IN A SUPERSONIC CONICAL FLOW
BROWNE, SH
FRIEDMAN, L
HODES, I
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (08): : 443 - 452
[3] PROBLEM OF MINIMAL DRAG OF CONICAL SUPERSONIC WING SURFACES WITH SUBSONIC LEADING EDGES
WAGNER, B
[J]. INGENIEUR ARCHIV, 1976, 45 (03): : 179 - 191
[4] A NOTE ON THE DRAG OF WING-BODY COMBINATIONS IN LINEARISED SUPERSONIC FLOW
FRAENKEL, LE
[J]. AERONAUTICAL QUARTERLY, 1958, 9 (03): : 305 - 311
[5] MINIMUM DRAG CAMBERED RECTANGULAR WING FOR SUPERSONIC SPEEDS
ROTT, N
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (09): : 642 - 643
[6] WING AND CONICAL BODY OF ARBITRARY CROSS-SECTION IN SUPERSONIC-FLOW
MATEESCU, D
[J]. JOURNAL OF AIRCRAFT, 1987, 24 (04): : 239 - 247
[7] Supersonic flow investigation of a drag reducing conical spike on a hemispherically blunted nose body
Sarwar, M. D. Gulam
Kumar, Priyank
Das, Sudip
[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (09) : 1992 - 2007
[8] Computation and visualization of the inviscid drag coefficient and polar surfaces of the wedged delta wing in supersonic flow
Nastase, A
Honermann, A
[J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1996, 76 : 629 - 630
[9] NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WING
BABAEV, DA
[J]. AIAA JOURNAL, 1963, 1 (09) : 2224 - 2231
[10] FLAT-TOP BODY OF MINIMUM DRAG FOR GIVEN LIFT AND LENGTH IN HYPERSONIC FLOW
LUSTY, AH
[J]. JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1967, 14 (02): : 82 - &

← 1 2 3 4 5 →