A numerical solution of the supersonic flow over a rearward facing step with transverse non-reacting hydrogen injection

Numerical solution for the inviscid supersonic flow in the corner formed by two intersecting wedges

10.2514/6.1973-675 ◽

1973 ◽

Cited By ~ 7

Author(s):

P. KUTLER

Keyword(s):

Supersonic Flow ◽

Numerical Solution

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Numerical solution of the problem of unsteady supersonic flow around the front part of the wings with a detached shock wave

Computer Methods in Applied Mechanics and Engineering ◽

10.1016/0045-7825(79)90078-1 ◽

1979 ◽

Vol 19 (2) ◽

pp. 257-275 ◽

Cited By ~ 3

Author(s):

G.P. Voskresensky

Keyword(s):

Shock Wave ◽

Supersonic Flow ◽

Numerical Solution ◽

Front Part ◽

Unsteady Supersonic Flow ◽

Detached Shock Wave

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On a numerical solution of related problems of supersonic flow over deformable shells of finite thickness

USSR Computational Mathematics and Mathematical Physics ◽

10.1016/0041-5553(87)90030-9 ◽

1987 ◽

Vol 27 (4) ◽

pp. 181-188 ◽

Cited By ~ 2

Author(s):

P.N. Korotin ◽

I.B. Petrov ◽

V.B. Pirogov ◽

A.S. Kholodov

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Finite Thickness

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Numerical solution of the problem of supersonic flow past conical bodies at an angle of attack

Fluid Dynamics ◽

10.1007/bf01016281 ◽

1967 ◽

Vol 1 (1) ◽

pp. 100-101

Author(s):

N. A. Makhin ◽

V. F. Syagaev

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Angle Of Attack ◽

Flow Past

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NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WING

AIAA Journal ◽

10.2514/3.2047 ◽

1963 ◽

Vol 1 (9) ◽

pp. 2224-2231 ◽

Cited By ~ 22

Author(s):

D. A. BABAEV

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Delta Wing ◽

Lower Surface ◽

Flow Past

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Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack

Computer Methods in Applied Mechanics and Engineering ◽

10.1016/s0045-7825(96)01203-0 ◽

1997 ◽

Vol 148 (1-2) ◽

pp. 11-21 ◽

Cited By ~ 1

Author(s):

E Qin ◽

Yang Guowei ◽

Li Fengwei

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

High Angles Of Attack

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Numerical solution of a problem involving the interaction of a shock wave with a cylinder in a supersonic flow

Journal of Engineering Physics ◽

10.1007/bf00835968 ◽

1971 ◽

Vol 21 (6) ◽

pp. 1518-1522 ◽

Cited By ~ 8

Author(s):

V. B. Balakin ◽

V. V. Bulanov

Keyword(s):

Shock Wave ◽

Supersonic Flow ◽

Numerical Solution

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The Numerical Solution of Certain Nonlinear Supersonic Flow Problems on the IBM Card Programmed Calculator

Journal of the Aeronautical Sciences (Institute of the Aeronautical Sciences) ◽

10.2514/8.2964 ◽

1954 ◽

Vol 21 (3) ◽

pp. 205-206

Author(s):

R. E. Bower ◽

J. H. Higman

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Flow Problems

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Numerical solution of the problem of supersonic flow past wings of arbitrary form with a detached shock wave

Eighth International Conference on Numerical Methods in Fluid Dynamics - Lecture Notes in Physics ◽

10.1007/3-540-11948-5_67 ◽

2008 ◽

pp. 513-518

Author(s):

G.P. Voskresensky

Keyword(s):

Shock Wave ◽

Supersonic Flow ◽

Numerical Solution ◽

Arbitrary Form ◽

Flow Past ◽

Detached Shock Wave

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Numerical solution of the problem of the supersonic flow of a gas from a plane slit in hodograph variables

USSR Computational Mathematics and Mathematical Physics ◽

10.1016/0041-5553(88)90224-8 ◽

1988 ◽

Vol 28 (1) ◽

pp. 93-96

Author(s):

Yu.S. Kosolapov

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Plane Slit

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