ANALYSIS OF SPIRALING VORTICAL FLOWS AROUND SLENDER DELTA WINGS MOVING IN AN INVISCID MEDIUM

被引：4

作者：

DAS, A

机构：

[1] DLR, Institut für Entwurfsaerodynamik, Braunschweig, W-3300

来源：

ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK | 1991年 / 71卷 / 11期

关键词：

D O I：

10.1002/zamm.19910711115

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

[No abstract available]

引用

页码：465 / 471

页数：7

共 27 条

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ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 2001, 81 : S413 - S414
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EKATERINARIS, JA
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[4] Numerical simulation of vortical flows over delta wings and analysis of vortex motion
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[5] Numerical computation of vortical flow fields of double-delta wings moving in a compressible viscous medium
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Zeitschrift fuer Angewandte Mathematik und Mechanik, 1994, 74 (10):
[6] Review of unsteady vortex flows over slender delta wings
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[8] THE CONTROL OF ASYMMETRIC VORTICAL FLOWS OVER DELTA WINGS AT HIGH ANGLES OF ATTACK
WOOD, NJ
ROBERTS, L
CELIK, Z
AIAA ATMOSPHERIC FLIGHT MECHANICS CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 484 - 491
[9] A VORTEX POINT METHOD FOR CALCULATION OF INVISCID INCOMPRESSIBLE FLOWS AROUND ROTARY WINGS
CANTALOUBE, B
HUBERSON, S
RECHERCHE AEROSPATIALE, 1984, (06): : 403 - 415
[10] Inviscid vortex structures in the shock layers of conical flows around V wings
M. A. Zubin
F. A. Maksimov
N. A. Ostapenko
Fluid Dynamics, 2017, 52 : 424 - 441

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