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Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method AIAA-2001-2252

Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method AIAA-2001-2252
紙規格・テクニカルリポート類
Loh, Ching Y, Hultgren, Lennart S, Jorgenson, Philip C. E2001<M-AIAA-2001-2252>
国立国会図書館

Measurements in separated and transitional boundary layers under low-pressure turbine airfoil conditions ASME-2000-GT-260

Measurements in separated and transitional boundary layers under low-pressure turbine airfoil conditions ASME-2000-GT-260
紙規格・テクニカルリポート類
Volino, Ralph J, Hultgren, Lennart S2000<M-ASME-2000-GT-260>
国立国会図書館

Predictions of separated and transitional boundary layers under low-pressure turbine airfoil conditions using an intermittency transport equation AIAA-2001-0446

Predictions of separated and transitional boundary layers under low-pressure turbine airfoil conditions using an intermittency transport equation AIAA-2001-0446
紙規格・テクニカルリポート類
Suzen, Y. Bora, Huang, P. G, Hultgren, Lennart S, Ashpis, David E2001<M-AIAA-2001-0446>
国立国会図書館

Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method [microform] / Ching Y. Loh, Lennart S. Hultgren, Philip C.E. Jorgenson ([NASA technical memorandum] ; NASA/TM-2001-210958)

Near field screech noise computation for an underexpanded supersonic jet by the CE/SE method [microform] / Ching Y. Loh, Lennart S. Hultgren, Philip C.E. Jorgenson ([NASA technical memorandum] ; NASA/TM-2001-210958)
マイクロ図書
2001<YCA-NAS 1.15:210958>
国立国会図書館
  • 著者標目Loh, Ching Y Hultgren, Lennart S Jorgenson, Philip C. E NASA G...

Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method AIAA-2000-0475

Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method AIAA-2000-0475
紙規格・テクニカルリポート類
Loh, Ching Y, Hultgren, Lennart S, Chang, Sin-Chung, Jorgenson, Philip C. E2000<M-AIAA-2000-0475>
国立国会図書館

Vortex dynamics simulation in aeroacoustics by the space-time conservation element and solution element method AIAA-99-0359

Vortex dynamics simulation in aeroacoustics by the space-time conservation element and solution element method AIAA-99-0359
紙規格・テクニカルリポート類
Loh, Ching Y, Hultgren, Lennart S, Chang, Sin-Chung, Jorgenson, Philip C. E1999<M-AIAA-99-0359>
国立国会図書館

Computing waves in compressible flow using the space-time conservation element and solution element method AIAA-98-0369

Computing waves in compressible flow using the space-time conservation element and solution element method AIAA-98-0369
紙規格・テクニカルリポート類
Loh, Ching Y, Hultgren, Lennart S, Chang, Sin-Chung1998<M-AIAA-98-0369>
国立国会図書館

Demonstration of separation delay with glow-discharge plasma actuators [microform] / Lennart S. Hultgren and David E. Ashpis (NASA/CR-2003-212204)

Demonstration of separation delay with glow-discharge plasma actuators [microform] / Lennart S. Hultgren and David E. Ashpis (NASA/CR-2003-212204)
マイクロ図書
2003<YCA-NAS 1.15:212204>
国立国会図書館
  • 著者標目Hultgren, Lennart S. (Lennart Sven) Ashpis, D. E....

A 3-D CE/SE Navier-Stokes solver with unstructured hexahedral grid for computation of near field jet screech noise [microform] / Ching Y. Loh and Ananda Himansu, Lennart S. Hultgren (NASA/TM-2003-212314)

A 3-D CE/SE Navier-Stokes solver with unstructured hexahedral grid for computation of near field jet screech noise [microform] / Ching Y. Loh and Ananda Himansu, Lennart S. Hultgren (NASA/TM-2003-212314)
マイクロ図書
2003<YCA-NAS 1.15:212314>
国立国会図書館
  • 著者標目...imansu, Ananda Hultgren, Lennart S. (Lennart Sven) NASA Glenn Re...

Computing jet screech--a complex aeroacoustic feedback system [microform] / Ching Y. Loh, Lennart S. Hultgren (NASA/TM-2002-211807)

Computing jet screech--a complex aeroacoustic feedback system [microform] / Ching Y. Loh, Lennart S. Hultgren (NASA/TM-2002-211807)
マイクロ図書
2002<YCA-NAS 1.15:2002-211807>
国立国会図書館
  • 著者標目Loh, Ching Y. (Ching Yuen) , 1944- Hultgren, Lennart S. (Lennart Sven) NASA Glenn Re...

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