Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by Crossref.
1962.
Hypersonic Flow Research.
p.
547.
Bray, K.N.C.
1962.
Hypersonic Flow Research.
p.
547.
JUNGOWSKI, W.M.
1964.
Fluid Dynamics Transactions.
p.
189.
Stalker, R. J.
1965.
An approximate theory of gun tunnel behaviour.
Journal of Fluid Mechanics,
Vol. 22,
Issue. 04,
p.
657.
Peng, Tzy C.
and
Elbert, Theo. F.
1965.
On the Piston Motion of a Free-Piston Shock Tube.
Aeronautical Quarterly,
Vol. 16,
Issue. 4,
p.
369.
Stalker, R. J.
1966.
The Free-Piston Shock Tube.
Aeronautical Quarterly,
Vol. 17,
Issue. 4,
p.
351.
KNOOS, STELLAN
1968.
Bypass piston tube, a new device for generating high temperatures and pressures in gases..
AIAA Journal,
Vol. 6,
Issue. 4,
p.
632.
Alkidas, A. C.
Plett, E. G.
and
Summerfield, M.
1976.
Performance study of a ballistic compressor.
AIAA Journal,
Vol. 14,
Issue. 12,
p.
1752.
Kimura, Takeyoshi
Kuwata, Chiaki
and
Nadai, Yoshikazu
1978.
Optimum Operating Technique of Two -S t age Hypersonic Gun Tunnel.
AIAA Journal,
Vol. 16,
Issue. 11,
p.
1185.
MATSUDA, Atsushi
and
NAGATA, Kenji
2015.
Relationship between the Non-dimensional Piston Property and the Piston Trajectory in Gun Tunnel.
AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES,
Vol. 14,
Issue. 0,
p.
137.