Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Küchemann, D.
1965.
Hypersonic aircraft and their aerodynamic problems.
Progress in Aerospace Sciences,
Vol. 6,
Issue. ,
p.
271.
LANDAU, Z.
and
YENERIZ, M.
1965.
Parametric supersonic combustion ramjet engine optimization.
Vaglio-Laurin, Roberto
and
Finke, Reinald G.
1965.
Reusable Space Launch Vehicle Concepts: Outlook 1965.
Vol. 1,
Issue. ,
SLUTSKY, S.
TAMAGNO, J.
and
TRENTACOSTE, N.
1965.
Supersonic combustion in premixed hydrogen-air flows.
AIAA Journal,
Vol. 3,
Issue. 9,
p.
1599.
FAVIN, S.
and
SCHETZ, J.
1966.
The ignition of slot-injected gaseous hydrogen in a supersonic air stream.
Morgenthaler, John H.
and
Marchello, Joseph M.
1966.
Turbulent transport coefficients in supersonic flow.
International Journal of Heat and Mass Transfer,
Vol. 9,
Issue. 12,
p.
1401.
FERRI, A.
1966.
Review of scramjet propulsion technology.
DONALDSON, COLEMAN DUP.
and
GRAY, K. EVAN
1966.
Theoretical and experimental investigation of the compressible free mixing of two dissimilar gases..
AIAA Journal,
Vol. 4,
Issue. 11,
p.
2017.
BAUER, R.
1966.
A hypersonic ramjet analysis with premixed fuel combustion.
Francis, R. H.
1967.
Air-Breathing Reusable Launchers.
Vol. 1,
Issue. ,
Kremer, Hans
1967.
Mixing in a plane free-turbulent-jet diffusion flame.
Symposium (International) on Combustion,
Vol. 11,
Issue. 1,
p.
799.
Pergament, H.S.
and
Calcote, H.F.
1967.
Thermal and chemi-ionization processes in afterburning rocket exhausts.
Symposium (International) on Combustion,
Vol. 11,
Issue. 1,
p.
597.
GARZA, LUIS R.
and
DODGE, FRANKLIN T.
1967.
A comparison of flexible and rigid ring baffles for slosh suppression..
Journal of Spacecraft and Rockets,
Vol. 4,
Issue. 6,
p.
805.
SCAGGS, NORMAN E.
and
DUNN, ROBERT G.
1967.
Development of a facility for supersonic combustion simulation..
Journal of Spacecraft and Rockets,
Vol. 4,
Issue. 6,
p.
803.
Schetz, J.A.
and
Favin, S.
1967.
An analysis of the ignition of slot-injected gaseous hydrogen in a supersonic air stream.
Combustion and Flame,
Vol. 11,
Issue. 5,
p.
397.
FERRI, A.
1968.
Review of scramjet propulsion technology..
Journal of Aircraft,
Vol. 5,
Issue. 1,
p.
3.
Küchemann, D.
and
Weber, J.
1968.
5 An analysis of some performance aspects of various types of aircraft designed to fly over different ranges at different speeds.
Progress in Aerospace Sciences,
Vol. 9,
Issue. ,
p.
329.
KÜCHEMANN, D.
and
WEBER, J.
1968.
Vol. 9,
Issue. ,
p.
329.
Swithebank, J.
and
Chigier, N.A.
1969.
Vortex mixing for supersonic combustion.
Symposium (International) on Combustion,
Vol. 12,
Issue. 1,
p.
1153.
WATTON, A.
1969.
The fuel-mixing mechanism in diffusion-type supersonic combustion.