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

N. A. Makhin; V. F. Syagaev

doi:10.1007/bf01016281

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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Supersonic flow past a sharp cone oscillating about a zero angle of attack

Fluid Dynamics ◽

10.1007/bf02698661 ◽

1998 ◽

Vol 33 (6) ◽

pp. 913-923

Author(s):

Yu. M. Lipnitskii ◽

E. V. Matsyura ◽

A. N. Pokrovskii

Keyword(s):

Supersonic Flow ◽

Angle Of Attack ◽

Flow Past ◽

Sharp Cone

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Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection

Fluid Dynamics ◽

10.1007/bf01051695 ◽

1988 ◽

Vol 22 (5) ◽

pp. 737-742 ◽

Cited By ~ 1

Author(s):

V. A. Antonov ◽

A. M. Grishin ◽

F. M. Pakhomov

Keyword(s):

Supersonic Flow ◽

Angle Of Attack ◽

Flow Past ◽

Blunt Bodies

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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 of the viscous hypersonic flow past blunted conesat angle of attack

10.2514/6.1977-172 ◽

1977 ◽

Cited By ~ 1

Author(s):

A. KUMAR ◽

R. GRAVES, JR.

Keyword(s):

Numerical Solution ◽

Hypersonic Flow ◽

Angle Of Attack ◽

Flow Past ◽

Viscous Hypersonic Flow

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Numerical investigation of supersonic flow past blunt bodies of intricate shape at an angle of attack and slip angle

High Temperature ◽

10.1007/bf02756005 ◽

2000 ◽

Vol 38 (3) ◽

pp. 444-452

Author(s):

A. I. Borodin ◽

S. V. Peigin

Keyword(s):

Supersonic Flow ◽

Numerical Investigation ◽

Angle Of Attack ◽

Slip Angle ◽

Flow Past ◽

Intricate Shape ◽

Blunt Bodies

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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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Supersonic flow past a star-shaped body without symmetry planes at angle of attack

Fluid Dynamics ◽

10.1007/bf01342693 ◽

1993 ◽

Vol 28 (4) ◽

pp. 560-567

Author(s):

M. I. Follet

Keyword(s):

Supersonic Flow ◽

Angle Of Attack ◽

Shaped Body ◽

Flow Past

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Flow past a slim body of revolution of a stationary supersonic flow of a vibrationally excited gas under a small angle of attack

Journal of Applied Mechanics and Technical Physics ◽

10.1007/bf00864780 ◽

1993 ◽

Vol 34 (3) ◽

pp. 304-312

Author(s):

A. N. Bogdanov ◽

V. A. Kulikovskii

Keyword(s):

Supersonic Flow ◽

Small Angle ◽

Angle Of Attack ◽

Body Of Revolution ◽

Vibrationally Excited ◽

Flow Past

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A scheme for computing near-axisymmetric gas flow and supersonic flow past a cylinder end-face at a low angle of attack

USSR Computational Mathematics and Mathematical Physics ◽

10.1016/0041-5553(86)90137-0 ◽

1986 ◽

Vol 26 (3) ◽

pp. 200-203

Author(s):

E.F. Zhigalko

Keyword(s):

Supersonic Flow ◽

Gas Flow ◽

Angle Of Attack ◽

Flow Past ◽

Flow Past A Cylinder

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Influence of the angle of attack on the transition from a laminar to a turbulent boundary layer in the case of supersonic flow past sharp circular cones

Fluid Dynamics ◽

10.1007/bf01090036 ◽

1983 ◽

Vol 17 (4) ◽

pp. 622-625

Author(s):

A. Ya. Yushin

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Angle Of Attack ◽

Flow Past

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