Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
HOLT, MAURICE
1961.
Direct Calculation of Pressure Distribution on Blunt Hypersonic Nose Shapes With Sharp Corners.
Journal of the Aerospace Sciences,
Vol. 28,
Issue. 11,
p.
872.
1961.
Publication/Subscription/Member Data.
Journal of the Aerospace Sciences,
Vol. 28,
Issue. 11,
p.
876.
Friedman, Manfred P.
1962.
Two-Dimensional and Axisymmetric Rotational Flows Past a Transonic Corner.
Journal of the Aerospace Sciences,
Vol. 29,
Issue. 4,
p.
503.
PROSNAK, W.J.
1965.
Fluid Dynamics Transactions.
p.
457.
Fal'kovich, S.V.
and
Chernov, I.A.
1966.
Algebraic self-modeling solutions of two-dimensional transonic gas flow.
Journal of Applied Mathematics and Mechanics,
Vol. 30,
Issue. 5,
p.
1004.
BOHACHEVSKY, IHOR O.
and
MATES, ROBERT E.
1966.
A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack..
AIAA Journal,
Vol. 4,
Issue. 5,
p.
776.
Belotserkovskii, O.M.
Sedova, E.S.
and
Shugaev, F.V.
1966.
The supersonic flow round blunt bodies of revolution with a break in the generator.
USSR Computational Mathematics and Mathematical Physics,
Vol. 6,
Issue. 5,
p.
210.
MESSITER, A.
and
OLSSON, G.
1968.
The hypersonic laminar boundary layer approaching the base of a slender body.
Belotserkovskii, O.M.
and
Shifrin, E.G.
1969.
Transonic flows behind a receding shock wave.
USSR Computational Mathematics and Mathematical Physics,
Vol. 9,
Issue. 4,
p.
230.
OLSSON, G. R.
and
MESSITER, A. F.
1969.
Hypersonic laminar boundary layer approaching the base of a slender body..
AIAA Journal,
Vol. 7,
Issue. 7,
p.
1261.
FISHBURN, B. D.
and
ADAMSON, T. C.
1972.
Transonic Region of a Supersonic Boundary Layer Turning a Sharp Corner.
AIAA Journal,
Vol. 10,
Issue. 2,
p.
123.
Lifshits, Yu. B.
and
Shifrin, �. G.
1973.
The problem of transonic flow past a convex body.
Fluid Dynamics,
Vol. 6,
Issue. 2,
p.
236.
Sevost'yanov, G. D.
1975.
Two-dimensional transonic vortex flows of an ideal gas.
Fluid Dynamics,
Vol. 8,
Issue. 5,
p.
767.
Shifrin, �. G.
1976.
Compression shock in the transonic flow around a convex corner.
Fluid Dynamics,
Vol. 9,
Issue. 5,
p.
712.
Minostsev, V. B.
1977.
Pressure gradient at a knee or discontinuity in the profile of blunted cones and wedges in supersonic flow.
Fluid Dynamics,
Vol. 12,
Issue. 1,
p.
91.
Diesperov, V.N.
1980.
The transonic flow of gas over a convex corner.
Journal of Applied Mathematics and Mechanics,
Vol. 44,
Issue. 1,
p.
38.
Ivanov, V.A.
and
Chernov, I.A.
1980.
An example of transonic flow past a body with discontinuity in the body profile curvature.
Journal of Applied Mathematics and Mechanics,
Vol. 44,
Issue. 5,
p.
675.
Diesperov, V.N.
1981.
Transonic rarefaction flow in the neighborhood of a convex corner.
Journal of Applied Mathematics and Mechanics,
Vol. 45,
Issue. 4,
p.
478.
Diesperov, V. N.
1984.
Transonic flow past a convex corner with free streamline.
Fluid Dynamics,
Vol. 18,
Issue. 5,
p.
769.
Kraiko, A.N.
Tillyaeva, N.I.
and
Shcherbakov, S.A.
1986.
A method of computing ideal gas flows in plane and axisymmetric nozzles with contour breaks.
USSR Computational Mathematics and Mathematical Physics,
Vol. 26,
Issue. 6,
p.
50.