Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by Crossref.
REASENBERG, ROBERT
1972.
Filtering with Perfectly Correlated Measurement Noise.
AIAA Journal,
Vol. 10,
Issue. 7,
p.
942.
CHOPRA, M. G.
1972.
Pressure Distribution on a Yawed Wedge Interacted by an Oblique Shock.
AIAA Journal,
Vol. 10,
Issue. 7,
p.
940.
Bernard, Peter S.
and
Berger, Bruce S.
1984.
Balance of Turbulent Energy in the Linear Wall Region of Channel Flow.
AIAA Journal,
Vol. 22,
Issue. 2,
p.
306.
Srivastava, R. S.
and
Deschambault, R. L.
1984.
Pressure Distribution Behind a Nonstationary Reflected-Diffracted Oblique Shock Wave.
AIAA Journal,
Vol. 22,
Issue. 2,
p.
305.
1986.
Gasdynamics.
p.
347.
Ben-Dor, Gabi
1992.
Shock Wave Reflection Phenomena.
p.
272.
Srivastava, R. S.
1994.
Interaction of Shock Waves.
Vol. 22,
Issue. ,
p.
73.
Srivastava, R. S.
1994.
Interaction of Shock Waves.
Vol. 22,
Issue. ,
p.
187.
Li, H
Ben-Dor, G
and
Han, Z Y
1994.
Analytical prediction of the reflected-diffracted shock wave shape in the interaction of a regular reflection with an expansive corner.
Fluid Dynamics Research,
Vol. 14,
Issue. 5,
p.
229.
Srivastava, R. S.
1994.
Interaction of Shock Waves.
Vol. 22,
Issue. ,
p.
1.
Srivastava, R. S.
1995.
Starting point of curvature for reflected diffracted shock wave.
AIAA Journal,
Vol. 33,
Issue. 11,
p.
2230.
Srivastava, R. S.
2007.
Effect of yaw on the starting point of curvature for reflected diffracted shock wave (subsonic and sonic cases).
Shock Waves,
Vol. 17,
Issue. 3,
p.
209.
Srivastava, RS
2018.
On the curvature of reflected diffracted shock wave interacted by an yawed wedge (Subsonic case).
Aeronautics and Aerospace Open Access Journal,
Vol. 2,
Issue. 3,