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1
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3943085501
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Navier-Stokes Analysis of an Ejector and Mixer-Ejector Operating at Pressure Ratios in the Range 2-4
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AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference, Orlando, Florida, July
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Malecki, R., Mityas, S., and Lord, W., "Navier-Stokes Analysis of an Ejector and Mixer-Ejector Operating at Pressure Ratios in the Range 2-4," AIAA 90-2730, AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference, Orlando, Florida, July 1990.
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AIAA 90-2730
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Malecki, R.1
Mityas, S.2
Lord, W.3
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2
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0020844260
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Numerical Study of the Turbulent Flow Past and Airfoil with Trailing Edge Separation
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November
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Rhie, C. M. & Chow, W. L., "Numerical Study of the Turbulent Flow Past and Airfoil with Trailing Edge Separation," AIAA J., Vol. 21, No. 11, November 1983, pp. 1525-1532
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The Prediction of Laminarization With a Two-Equation Model of Turbulence
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0003960347
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High Velocity Jet Noise Source Location and Reduction: Task 2-Theoretical Developments and Basic Experiments
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FAA-RD-76-79-II, May
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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.
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6
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0003957351
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Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle Using k-ε Turbulence Model
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AIAA 30th Aerospace Sciences Meeting, Reno, NV
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Khavaran, A., Krejsa, E. A., and Kim, C. M., "Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle Using k-ε Turbulence Model," AIAA 92-0500, AIAA 30th Aerospace Sciences Meeting, Reno, NV, 1992.
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AIAA 92-0500
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Khavaran, A.1
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Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle
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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.
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J. Wiley & Sons, New York, 19xx
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Richards, E. J., and Mead, D. J., Noise and Acoustic Fatigue in Aeronautics, J. Wiley & Sons, New York, 19xx, pp 139-141.
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9
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84964444614
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Flowfleld Measurements and Analysis of a 1/7-Scale Mixed Flow Exhaust System Model
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31st AIAA/ASME/SAE/ASME Joint Propulsion Conference, San Diego CA, July
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Zysman, S. H., Chiappetta, L. M., Saiyed, N. H., & Podboy, G. G., "Flowfleld Measurements and Analysis of a 1/7-Scale Mixed Flow Exhaust System Model," AIAA 95-2744, 31st AIAA/ASME/SAE/ASME Joint Propulsion Conference, San Diego CA, July 1995.
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AIAA 95-2744
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Zysman, S.H.1
Chiappetta, L.M.2
Saiyed, N.H.3
Podboy, G.G.4
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10
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84964458855
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Laser Doppler Velocimeter System for Subsonic Jet Mixer Nozzle Testing at the NASA Lewis Aeroacoustic Propulsion Lab
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31st AIAA/ASME/ SAE/ASME Joint Propulsion Conference, San Diego CA, July
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Podboy, G. G., Bridges, J., Saiyed, N. H., & Krupar, M., "Laser Doppler Velocimeter System for Subsonic Jet Mixer Nozzle Testing at the NASA Lewis Aeroacoustic Propulsion Lab," AIAA 95-2787, 31st AIAA/ASME/ SAE/ASME Joint Propulsion Conference, San Diego CA, July 1995.
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AIAA 95-2787
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Podboy, G.G.1
Bridges, J.2
Saiyed, N.H.3
Krupar, M.4
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11
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85006355563
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Computer-Aided Block-Structuring Through the Use of Optimization and Expert System Techniques
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AIAA 10th Computational Fluid Dynamics Conference, Honolulu, HI, June
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Dannenhoffer, J. F., Ill, "Computer-Aided Block-Structuring Through the Use of Optimization and Expert System Techniques," AIAA 91-1585, AIAA 10th Computational Fluid Dynamics Conference, Honolulu, HI, June 1991.
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AIAA 91-1585
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Dannenhoffer, J.F.1
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12
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0344370034
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A Block-Structuring Technique for General Geometries
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AIAA 29th Aerospace Sciences Meeting, Reno, NV, January
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Dannenhoffer, J. D., Ill, "A Block-Structuring Technique for General Geometries," AIAA 91-0145, AIAA 29th Aerospace Sciences Meeting, Reno, NV, January 1991.
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AIAA 91-0145
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13
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0026169502
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The Analysis and Modeling of Dilatational Terms in Compressible Turbulence
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14
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85007040130
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A Numerical Method for Navier-Stokes Equations with Finite Rate Chemistry
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AIAA 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference, June 1989, Buffalo, NY
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Choi, D., Weeratunga, S. and Knight, C.J., "A Numerical Method for Navier-Stokes Equations with Finite Rate Chemistry," AIAA-89-1857, AIAA 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference, June 1989, Buffalo, NY.
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Choi, D.1
Weeratunga, S.2
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15
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85002515883
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Experimental Investigation of Shock-Cell Noise Reduction for Single Stream Nozzles in Simulated Flight, Comprehensive Data Report, Vols. 1-3
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NASA CR-168234
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Yamamoto, K.1
Brausch, J.F.2
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16
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84889515253
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Application of an RNG k-ε Model to Compressible Turbulent Shear Layers
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June 1993, also AIAA 94-0188, 32nd Aerospace Sciences Meeting, Reno NV
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Choi, D., Sabnis, J. S. and Barber, T. J., "Application of an RNG k-ε Model to Compressible Turbulent Shear Layers," UTRC Report 93-25, June 1993, also AIAA 94-0188, 32nd Aerospace Sciences Meeting, Reno NV, 1994.
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Choi, D.1
Sabnis, J.S.2
Barber, T.J.3
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17
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33645384961
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On the Scaling of Small-Scale Jet Noise to Large Scale
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DGLR/AIAA 14th Aeroacoustics Conference, Aachen, Germany
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Soderman, P. T., "On the Scaling of Small-Scale Jet Noise to Large Scale," DGLR/AIAA 92-02-109, DGLR/AIAA 14th Aeroacoustics Conference, Aachen, Germany, 1992, p. 663.
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DGLR/AIAA 92-02-109
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Soderman, P.T.1
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18
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Hush Kit Directional Microphone Acoustic Test
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Simonich, J., "Hush Kit Directional Microphone Acoustic Test," UTRC Report 90-30, August 17, 1990.
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UTRC Report 90-30
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