-
1
-
-
0030797965
-
Sound Generation in a Mixing Layer
-
Colonius, T., Lele, S. K., and Moin, P., Sound Generation in a Mixing Layer, J. Fluid Mechanics, Vol. 330, 1997, pp. 375-409.
-
(1997)
J. Fluid Mechanics
, vol.330
, pp. 375-409
-
-
Colonius, T.1
Lele, S.K.2
Moin, P.3
-
2
-
-
0003960347
-
-
Federal Aviation Administration, FAA-RD-76-79-II, May
-
Mani, R., Balsa, T. E., Gliebe, P. R., et al., High Velocity Jet Noise Source Location and Reduction: Task 2-Theoretical Developments and Basic Experiments, Federal Aviation Administration, FAA-RD-76-79-II, May 1978.
-
(1978)
High Velocity Jet Noise Source Location and Reduction: Task 2-Theoretical Developments and Basic Experiments
-
-
Mani, R.1
Balsa, T.E.2
Gliebe, P.R.3
-
3
-
-
0003957351
-
-
AIAA 92-0500, AIAA 30th Aerospace Sciences Meeting, Reno, NV
-
Khavaran, A., Krejsa, E. A., and Kim, C. M., Computation of Supersonic Jet Mixing Noise for an Axisymmetric C-D Nozzle Using k-e Turbulence Model, AIAA 92-0500, AIAA 30th Aerospace Sciences Meeting, Reno, NV, 1992.
-
(1992)
Computation of Supersonic Jet Mixing Noise For An Axisymmetric C-D Nozzle Using K-e Turbulence Model
-
-
Khavaran, A.1
Krejsa, E.A.2
Kim, C.M.3
-
4
-
-
0028429704
-
Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle
-
Khavaran, A., Krejsa, E. A., and Kim, C. M., Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle, Journal of Aircraft, Vol. 31, No. 3,1994, p. 603.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.3
, pp. 603
-
-
Khavaran, A.1
Krejsa, E.A.2
Kim, C.M.3
-
5
-
-
0028496130
-
Significance of Shock Structure on Supersonic Jet Mixing of Axisymmetric Nozzles
-
Sept
-
Kim, C. M., Krejsa, E. A., and Khavaran, A., Significance of Shock Structure on Supersonic Jet Mixing of Axisymmetric Nozzles, AIAA Journal, Vol. 32, No. 9, Sept. 1994, pp. 1920-1923.
-
(1994)
AIAA Journal
, vol.32
, Issue.9
, pp. 1920-1923
-
-
Kim, C.M.1
Krejsa, E.A.2
Khavaran, A.3
-
6
-
-
0033165089
-
On the Role of Anisotropy in Turbulent Mixing Noise
-
th AIAA/CEAS Aeroacoustics Conference, Toulouse, France, June 2-4, 1998
-
th AIAA/CEAS Aeroacoustics Conference, Toulouse, France, June 2-4, 1998.
-
(1999)
AIAA Journal
, vol.37
, Issue.7
-
-
Khavaran, A.1
Krejsa, E.A.2
-
8
-
-
17144432829
-
Centerline Velocity Decay of Compressible Free Jets
-
Witze, P. O., Centerline Velocity Decay of Compressible Free Jets, AIAA Journal, Vol. 12, pp. 417-418, 1974.
-
(1974)
AIAA Journal
, vol.12
, pp. 417-418
-
-
Witze, P.O.1
-
9
-
-
0000470914
-
On Sound Generated Aerodynamically: I. General Theory
-
Lighthill, M. J., On Sound Generated Aerodynamically: I. General Theory, Proceedings of the Royal Society, Vol. 211 A, pp. 564-587, 1952.
-
(1952)
Proceedings of the Royal Society
, vol.211
, pp. 564-587
-
-
Lighthill, M.J.1
-
11
-
-
0021124056
-
Aeroacoustics and turbulent shear flows
-
Goldstein, M. E., Aeroacoustics and turbulent shear flows, Ann. Rev. Fluid Mechanics, Vol. 16, 1984, pp. 263-285.
-
(1984)
Ann. Rev. Fluid Mechanics
, vol.16
, pp. 263-285
-
-
Goldstein, M.E.1
-
13
-
-
0014557550
-
Quadrupole Corrections Governing the Pattern of Jet Noise
-
Ribner, H. S., Quadrupole Corrections Governing the Pattern of Jet Noise, J. Fluid Mechanics, Vol. 38, 1969, p. 1
-
(1969)
J. Fluid Mechanics
, vol.38
, pp. 1
-
-
Ribner, H.S.1
-
14
-
-
5244246831
-
-
NASA CR-3845, December
-
Yamamoto, K., Brausch, J. F., Balsa, T. F., et al., Experimental Investigation of Shock-Cell Noise Reduction for Single Stream Nozzles in Simulated Flight, NASA CR-3845, December 1984.
-
(1984)
Experimental Investigation of Shock-Cell Noise Reduction For Single Stream Nozzles In Simulated Flight
-
-
Yamamoto, K.1
Brausch, J.F.2
Balsa, T.F.3
-
15
-
-
0031272223
-
An Assessment of Jet Noise Analysis Codes for Multistream Axisymmetric & Forced Mixer Nozzles
-
AIAA 96-0750, AIAA 34th Aerospace Sciences Meeting, Reno NV, 1996
-
Barber, T. J., Chiappetta, L. M., and Zysman, S. H., An Assessment of Jet Noise Analysis Codes for Multistream Axisymmetric & Forced Mixer Nozzles, AIAA 96-0750, AIAA 34th Aerospace Sciences Meeting, Reno NV, 1996, also AIAA Journal for Propulsion and Power, Vol. 13, No. 6, 1997, pp. 737-744.
-
(1997)
AIAA Journal For Propulsion and Power
, vol.13
, Issue.6
, pp. 737-744
-
-
Barber, T.J.1
Chiappetta, L.M.2
Zysman, S.H.3
-
16
-
-
84897874782
-
-
AIAA 2000-2022, 6th AIAA/CEAS Aeroacoustics conference, Maui, HA, June
-
Simonich, J., Narayanan, S., Barber, T.J. & Kudo, T., High Subsonic Jet Experiments Part I: Aeroacoustic Characterization, Noise Reduction and Dimensional Scaling Effects, AIAA 2000-2022, 6th AIAA/CEAS Aeroacoustics conference, Maui, HA, June 2000.
-
(2000)
High Subsonic Jet Experiments Part I: Aeroacoustic Characterization, Noise Reduction and Dimensional Scaling Effects
-
-
Simonich, J.1
Narayanan, S.2
Barber, T.J.3
Kudo, T.4
-
17
-
-
84894632470
-
-
AIAA 2000-2023, 6th AIAA/CEAS Aeroacoustics Conference, Lahaina, Hawaii, June 12-14
-
Narayanan, S., Barber, T. and Polak, D., High Subsonic Jet Experiments Part II: Turbulence and Noise Generation Studies, AIAA 2000-2023, 6th AIAA/CEAS Aeroacoustics Conference, Lahaina, Hawaii, June 12-14, 2000.
-
(2000)
High Subsonic Jet Experiments Part II: Turbulence and Noise Generation Studies
-
-
Narayanan, S.1
Barber, T.2
Polak, D.3
-
18
-
-
0027545120
-
Application of Scalar Implicit Approximate Factor-ization for an Underwater Magneto-Hydrodynamic Propulsion System Analysis
-
Feb
-
Choi, D. and Knight, C. J., Application of Scalar Implicit Approximate Factor-ization for an Underwater Magneto-Hydrodynamic Propulsion System Analysis, AIAA Journal, Vol.31, No.2, pp. 286-293, Feb 1993.
-
(1993)
AIAA Journal
, vol.31
, Issue.2
, pp. 286-293
-
-
Choi, D.1
Knight, C.J.2
-
19
-
-
85007040130
-
A Numerical Method for Navier-Stokes Equations with Finite Rate Chemistry
-
Buffalo, New York, June
-
Choi, D., Weeratunga, S. and Knight C. J., A Numerical Method for Navier-Stokes Equations with Finite Rate Chemistry, AIAA-98-1857, AlAA/ASME 7th Fluid Mechanics, Plasma Dynamics and Materials Conference, Buffalo, New York, June 1989.
-
(1989)
AIAA-98-1857, AlAA/ASME 7th Fluid Mechanics, Plasma Dynamics and Materials Conference
-
-
Choi, D.1
Weeratunga, S.2
Knight, C.J.3
-
20
-
-
0020844260
-
Numerical Study of the Turbulent Flow Past and Airfoil with Trailing Edge Separation
-
November
-
Rhie, C. M. & Chow, W. L., Numerical Study of the Turbulent Flow Past and Airfoil with Trailing Edge Separation, AIAA Journal, Vol. 21, No. 11, November 1983, pp. 1525-1532.
-
(1983)
AIAA Journal
, vol.21
, Issue.11
, pp. 1525-1532
-
-
Rhie, C.M.1
Chow, W.L.2
|