Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Rott, N.
and
Thomann, H.
1971.
Finite-amplitude and diffusive effects in acoustics: a report on EUROMECH 23.
Journal of Fluid Mechanics,
Vol. 49,
Issue. 2,
p.
391.
Brocher, E.
and
Maresca, C.
1973.
Etude des phenomenes thermiques dans un tube de Hartmann-Sprenger.
International Journal of Heat and Mass Transfer,
Vol. 16,
Issue. 3,
p.
529.
MARCHESE, V. P.
RAKOWSKY, E. L.
and
BEMENT, L. J.
1973.
A Fluidic Sounding Rocket Motor Ignition System.
Journal of Spacecraft and Rockets,
Vol. 10,
Issue. 11,
p.
731.
MARTLEW, D.
1975.
The use of Hartmann generators as sources of high intensity sound ina large absorption flow duct facility.
Brocher, Eric
and
Maresca, Christian
1975.
Comment on "Experimental Investigation of a Cylindrical Resonator ".
AIAA Journal,
Vol. 13,
Issue. 8,
p.
1127a.
Brocher, Eric
1975.
Heating Rate of the Driven Gas in a Hartmann-Sprenger Tube.
AIAA Journal,
Vol. 13,
Issue. 10,
p.
1265.
Brocher, Eric
and
Betton, Michel
1975.
Experiments with the hydraulic analogy of a shock-wave magnetohydrodynamic generator.
The Physics of Fluids,
Vol. 18,
Issue. 7,
p.
795.
Wu, J. H.T.
Ostrowski, P. P.
Neemeh, R. A.
and
Lee, P.H.W.
1975.
Reply by Authors to E. Brocher and C. Maresca.
AIAA Journal,
Vol. 13,
Issue. 8,
p.
1127b.
1976.
Aeroacoustics: Acoustic Wave Propagation; Aircraft Noise Prediction; Aeroacoustic Instrumentation.
p.
203.
Przirembel, C.E. G.
and
Fletcher, L. S.
1978.
Aerothermodynamic Characteristics of a Resonance Tube Driven by a Subsonic Jet.
AIAA Journal,
Vol. 16,
Issue. 2,
p.
184.
Wu, J.H.T.
Ostrowski, P.P.
and
Neemeh, R.A.
1978.
Acoustic performance of a cylindrical disk-type resonator.
Journal of Sound and Vibration,
Vol. 60,
Issue. 1,
p.
151.
Jungowski, W.M.
1979.
Some self induced supersonic flow oscillations.
Progress in Aerospace Sciences,
Vol. 18,
Issue. ,
p.
151.
Vagramenko, Ya. A.
Lyakhov, V. N.
and
Ustinov, V. M.
1979.
Pulsating regime corresponding to an obstacle in a stationary inhomogeneous flow.
Fluid Dynamics,
Vol. 14,
Issue. 5,
p.
686.
Przirembel, C. E. G.
1980.
Aerothermodynamic Aspects of an I .5 Axisymmetric Resonance Tube.
AIAA Journal,
Vol. 18,
Issue. 9,
p.
1141.
Masaaki, Kawahashi
and
Makoto, Suzuki
1981.
Temperature separation produced by a Hartmann-Sprenger tube coupling a secondary resonator.
International Journal of Heat and Mass Transfer,
Vol. 24,
Issue. 12,
p.
1951.
Brocher, E.
and
Ardissone, J.-P.
1983.
Heating characteristics of a new type of Hartmann-Sprenger tube.
International Journal of Heat and Fluid Flow,
Vol. 4,
Issue. 2,
p.
97.
Möhring, Willi
Müller, Ernst-August
and
Obermeier, Frank
1983.
Problems in flow acoustics.
Reviews of Modern Physics,
Vol. 55,
Issue. 3,
p.
707.
Rott, N.
1984.
Thermoacoustic heating at the closed end of an oscillating gas column.
Journal of Fluid Mechanics,
Vol. 145,
Issue. -1,
p.
1.
Brocher, E.
1985.
Flow of Real Fluids.
Vol. 235,
Issue. ,
p.
235.
Brocher, Eric
and
Duport, Elisabeth
1988.
Resonance tubes in a subsonic flowfield.
AIAA Journal,
Vol. 26,
Issue. 5,
p.
548.