-
1
-
-
0016127632
-
Measuring the combustion response of a forced oscillation method
-
BROWN R. S., ERICKSON J. E., BABCOCK W. R. Measuring the combustion response of a forced oscillation method. AIAA Journal. 12:1974;1502-1510.
-
(1974)
AIAA Journal
, vol.12
, pp. 1502-1510
-
-
Brown, R.S.1
Erickson, J.E.2
Babcock, W.R.3
-
3
-
-
0003595133
-
Coupling between velocity oscillations and solid propellant combustion
-
R. S. BROWN, A. M. BLACKNER, P. G. WILLOUGHBY, R. DUNLAP, 1986, AIAA Paper No. 86-0531, January, Coupling between velocity oscillations and solid propellant combustion.
-
(1986)
AIAA Paper No. 86-0531, January
-
-
Brown, R.S.1
Blackner, A.M.2
Willoughby, P.G.3
Dunlap, R.4
-
5
-
-
85007662794
-
Rotational axisymmetric mean flow and damping of acoustic waves in a solid propellant rocket
-
CULICK F. E. C. Rotational axisymmetric mean flow and damping of acoustic waves in a solid propellant rocket. AIAA Journal. 4:1966;1462-1464.
-
(1966)
AIAA Journal
, vol.4
, pp. 1462-1464
-
-
Culick, F.E.C.1
-
6
-
-
0024886189
-
Innovative method of investigating the role of turbulence in the velocity coupling phenomenon
-
New York: American Society of Mechanical Engineers. p. 17-22
-
MA Y., VAN MOORHEM W. K., SHORTHILL R. W. Innovative method of investigating the role of turbulence in the velocity coupling phenomenon. Combustion Instabilities Driven by Thermo-Chemical Acoustic Sources. 1989;American Society of Mechanical Engineers, New York. p. 17-22.
-
(1989)
Combustion Instabilities Driven by Thermo-Chemical Acoustic Sources
-
-
Ma, Y.1
Van Moorhem, W.K.2
Shorthill, R.W.3
-
7
-
-
0040824663
-
A simulation of the flow near a burning propellant in a solid propellant rocket motor
-
MA Y. A simulation of the flow near a burning propellant in a solid propellant rocket motor. Ph.D. Thesis, University of Utah, Salt Lake City. 1990.
-
(1990)
Ph.D. Thesis, University of Utah, Salt Lake City
-
-
Ma, Y.1
-
10
-
-
0040801190
-
Improved flowfield models in rocket motors and the Stokes layer with sidewall injection
-
MAJDALANI J. Improved flowfield models in rocket motors and the Stokes layer with sidewall injection. Ph.D. Thesis, University of Utah, Salt Lake City, UT. 1995.
-
(1995)
Ph.D. Thesis, University of Utah, Salt Lake City, UT
-
-
Majdalani, J.1
-
11
-
-
0002060373
-
Asymptotic formulation for an acoustically driven field inside a rectangular cavity with a well-defined convective mean flow motion
-
MAJDALANI J. Asymptotic formulation for an acoustically driven field inside a rectangular cavity with a well-defined convective mean flow motion. Journal of Sound and Vibration. 223:1999;73-95.
-
(1999)
Journal of Sound and Vibration
, vol.223
, pp. 73-95
-
-
Majdalani, J.1
-
14
-
-
0024882031
-
Effects of vorticity transport on axial acoustic waves in a solid propellant rocket chamber
-
New York: American Society of Mechanical Engineers. p. 53-61
-
FLANDRO G. A. Effects of vorticity transport on axial acoustic waves in a solid propellant rocket chamber. Combustion Instabilities Driven by Thermo-Chemical Acoustic Sources. 1989;American Society of Mechanical Engineers, New York. p. 53-61.
-
(1989)
Combustion Instabilities Driven by Thermo-Chemical Acoustic Sources
-
-
Flandro, G.A.1
-
15
-
-
0002581897
-
The transverse velocity gradient near the mouths of pipes in which an alternating or continuous flow of air is established
-
RICHARDSON E. G., TYLER E. The transverse velocity gradient near the mouths of pipes in which an alternating or continuous flow of air is established. Proceedings of the Royal Society, London. A 42:1929;1-15.
-
(1929)
Proceedings of the Royal Society, London
, vol.42
, pp. 1-15
-
-
Richardson, E.G.1
Tyler, E.2
-
16
-
-
0022812699
-
Injection-induced flows in porous-walled ducts
-
BEDDINI R. A. Injection-induced flows in porous-walled ducts. AIAA Journal. 24:1986;1766-1773.
-
(1986)
AIAA Journal
, vol.24
, pp. 1766-1773
-
-
Beddini, R.A.1
-
17
-
-
0024055798
-
Turbularization of an acoustic boundary layer on a transpiring surface
-
BEDDINI R. A., ROBERTS T. A. Turbularization of an acoustic boundary layer on a transpiring surface. AIAA Journal. 26:1988;917-923.
-
(1988)
AIAA Journal
, vol.26
, pp. 917-923
-
-
Beddini, R.A.1
Roberts, T.A.2
-
18
-
-
0026835325
-
Response of propellant combustion to a turbulent acoustic boundary layer
-
BEDDINI R. A., ROBERTS T. A. Response of propellant combustion to a turbulent acoustic boundary layer. Journal of Propulsion and Power. 8:1992;290-296.
-
(1992)
Journal of Propulsion and Power
, vol.8
, pp. 290-296
-
-
Beddini, R.A.1
Roberts, T.A.2
-
19
-
-
0024771462
-
Numerical study of turbulent reacting flows in solid-propellant ducted rocket combustors
-
CHERNG D. L., YANG V., KUO K. K. Numerical study of turbulent reacting flows in solid-propellant ducted rocket combustors. Journal of Propulsion and Power. 5:1989;678-685.
-
(1989)
Journal of Propulsion and Power
, vol.5
, pp. 678-685
-
-
Cherng, D.L.1
Yang, V.2
Kuo, K.K.3
-
20
-
-
0026835326
-
Numerical study of solid-fuel combustion under supersonic crossflows
-
JARYMOWYCZ T. A., YANG V., KUO K. K. Numerical study of solid-fuel combustion under supersonic crossflows. Journal of Propulsion and Power. 8:1992;346-353.
-
(1992)
Journal of Propulsion and Power
, vol.8
, pp. 346-353
-
-
Jarymowycz, T.A.1
Yang, V.2
Kuo, K.K.3
-
21
-
-
0028385289
-
Combustion of a double-base homogeneous propellant in a rocket motor
-
TSENG I. S., YANG V. Combustion of a double-base homogeneous propellant in a rocket motor. Combustion & Flame. 96:1994;325-342.
-
(1994)
Combustion & Flame
, vol.96
, pp. 325-342
-
-
Tseng, I.S.1
Yang, V.2
|