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Characteristics of residual mixing noise from internal fan/core mixers [microform] / Eugene A. Krejsa and Naseem H. Saiyed (NASA technical memorandum ; 107395)

Characteristics of residual mixing noise from internal fan/core mixers [microform] / Eugene A. Krejsa and Naseem H. Saiyed (NASA technical memorandum ; 107395)
マイクロ図書
1997<YCA-NAS 1.15:107395>
国立国会図書館
  • 著者標目Krejsa, E. A Saiyed, Naseem H United State...

Propogation of high frequency jet noise using geometric acoustics microform / A. Khavaran and (NASA technical memorandum ; 105950)

Propogation of high frequency jet noise using geometric acoustics microform / A. Khavaran and (NASA technical memorandum ; 105950)
マイクロ図書
1993<YCA-NAS 1.15:105950>
国立国会図書館
  • 著者標目Khavaran, A Krejsa, E. A United States. National Aeron...

Propagation of high frequency jet noise using geometric acoustics [microform] / A. Khavaran and E.A. Krejsa (NASA technical memorandum ; 106013)

Propagation of high frequency jet noise using geometric acoustics [microform] / A. Khavaran and E.A. Krejsa (NASA technical memorandum ; 106013)
マイクロ図書
1993<YCA-NAS 1.15:106013>
国立国会図書館
  • 著者標目Khavaran, A Krejsa, E. A United States. National Aeron...

Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-(epsilon) turbulence model microform / Abbas Khavaran and Eugene A. Krejsa and Chan M. Kim (NASA technical memorandum ; 105338)

Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-(epsilon) turbulence model microform / Abbas Khavaran and Eugene A. Krejsa and Chan M. Kim (NASA technical memorandum ; 105338)
マイクロ図書
1991<YCA-NAS 1.15:105338>
国立国会図書館
  • 著者標目Khavaran, Abbas Krejsa, E. A Kim, Chan M United States. Na...

Application of 3-Signal Coherence to Core Noise Transmission NASA-TM-83333 N83-23114 NAS-11583333 E-1580

Application of 3-Signal Coherence to Core Noise Transmission NASA-TM-83333 N83-23114 NAS-11583333 E-1580
マイクロ規格・テクニカルリポート類
Krejsa, E. A<LS-N83/23114>
国立国会図書館

Theoretical Model for the Cross Spectra Between Pressure and Temperature Downstream of a Combustor NASA-TM-83671 N84-34231 NAS-11583671 E-2114

Theoretical Model for the Cross Spectra Between Pressure and Temperature Downstream of a Combustor NASA-TM-83671 N84-34231 NAS-11583671 E-2114
マイクロ規格・テクニカルリポート類
Miles, J. H, Krejsa, E. A<LS-N84/34231>
国立国会図書館

Cross Spectra Between Pressure and Temperature in a Constant-Area Duct Downstream of a Hydrogen-Fueled Combustor NASA-TM-83463 N84-11885 NAS-11583463 E-1779

Cross Spectra Between Pressure and Temperature in a Constant-Area Duct Downstream of a Hydrogen-Fueled Combustor NASA-TM-83463 N84-11885 NAS-11583463 E-1779
マイクロ規格・テクニカルリポート類
Miles, J. H, Wasserbauer, C. A, Krejsa, E. A<LS-N84/11885>
国立国会図書館

Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle Using K-Epsilon Turbulence Model NASA-TM-105338 N92-14795 NAS-115105338 E-6705

Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle Using K-Epsilon Turbulence Model NASA-TM-105338 N92-14795 NAS-115105338 E-6705
マイクロ規格・テクニカルリポート類
Khavaran, A, Krejsa, E. A, Kim, C. M<LS-N92/14795>
国立国会図書館

Prediction of the Noise from a Propeller at Angle of Attack NASA-TM-103627 N91-11495 NAS-115103627 E-5795

Prediction of the Noise from a Propeller at Angle of Attack NASA-TM-103627 N91-11495 NAS-115103627 E-5795
マイクロ規格・テクニカルリポート類
Krejsa, E. A<LS-N91/11495>
国立国会図書館

Cross Spectra Between Temperature and Pressure in a Constant Area Duct Downstream of a Combustor NASA-TM-83351 N83-23116 NAS-11583351 E-1608

Cross Spectra Between Temperature and Pressure in a Constant Area Duct Downstream of a Combustor NASA-TM-83351 N83-23116 NAS-11583351 E-1608
マイクロ規格・テクニカルリポート類
Miles, J. H, Wasserbauer, C. A, Krejsa, E. A<LS-N83/23116>
国立国会図書館

Combustion Noise from Gas Turbine Aircraft Engines Measurement of Far-Field Levels NASA-TM-88971 N87-17480 NAS-11588971 E-3407

Combustion Noise from Gas Turbine Aircraft Engines Measurement of Far-Field Levels NASA-TM-88971 N87-17480 NAS-11588971 E-3407
マイクロ規格・テクニカルリポート類
Krejsa, E. A<LS-N87/17480>
国立国会図書館

Acoustical Modal Analysis of the Pressure Field in the Tailpipe of a Turbofan Engine NASA-TM-83387 N83-25499 NAS-11583387 E-1665

Acoustical Modal Analysis of the Pressure Field in the Tailpipe of a Turbofan Engine NASA-TM-83387 N83-25499 NAS-11583387 E-1665
マイクロ規格・テクニカルリポート類
Krejsa, E. A, Karchmer, A. M<LS-N83/25499>
国立国会図書館

Predicted and Measured Boundary Layer Refraction for Advanced Turboprop Propeller Noise NASA-TM-102365 N90-17413 NAS-115102365 E-5081

Predicted and Measured Boundary Layer Refraction for Advanced Turboprop Propeller Noise NASA-TM-102365 N90-17413 NAS-115102365 E-5081
マイクロ規格・テクニカルリポート類
Dittmar, J. H, Krejsa, E. A<LS-N90/17413>
国立国会図書館

Survey of the Broadband Shock Associated Noise Prediction Methods NASA-TM-105365 N92-14797 NAS-115105365 E-6743

Survey of the Broadband Shock Associated Noise Prediction Methods NASA-TM-105365 N92-14797 NAS-115105365 E-6743
マイクロ規格・テクニカルリポート類
Kim, C. M, Krejsa, E. A, Khavaran, A<LS-N92/14797>
国立国会図書館

Noise Measurements from an Ejector Suppressor Nozzle in the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel NASA-TM-103628 N91-11493 NAS-115103628 E-5717

Noise Measurements from an Ejector Suppressor Nozzle in the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel NASA-TM-103628 N91-11493 NAS-115103628 E-5717
マイクロ規格・テクニカルリポート類
Krejsa, E. A, Cooper, B. A, Hall, D. G, Khavaran, A<LS-N91/11493>
国立国会図書館

Identification and Proposed Control of Helicopter Transmission Noise at the Source NASA-TM-89312 N87-16816 NAS-11589312 USAAVCOMTR-87-C-2

Identification and Proposed Control of Helicopter Transmission Noise at the Source NASA-TM-89312 N87-16816 NAS-11589312 USAAVCOMTR-87-C-2
マイクロ規格・テクニカルリポート類
Coy, J. J, Handschuh, R. F, Lewicki, D. G, Huff, R. G, Krejsa, E. A<LS-N87/16816>
国立国会図書館

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