An Efficient and Robust Method for predicting Helicopter Rotor High-Speed Impulsive Noise | 東京工業大学附属図書館文献データベース

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An Efficient and Robust Method for predicting Helicopter Rotor High-Speed Impulsive Noise

著者名:: Brentner, Kenneth S. ( NASA langley Research Center )
掲載資料名:: NASA Technical Reports
発行年:: 1996
巻:: 19960016673
号:: NASA-TM-111251
パート:: NAS 1.15:111251
ペーパー番号:: N96-22286
開始ページ:: 1
終了ページ:: 16
総ページ数:: 16
出版情報:: National Aeronautics and Space Adminstration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:

ZA00001432

類似資料:

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3 テクニカルペーパー PREDICTION OF HELICOPTER ROTOR DISCRETE FREQUENCY NOISE: A COMPUTER PROGRAM INCORPORATING REALISTIC BLADE MOTIONS Brentner, K.S. National Aeronautics and Space Administration	9 テクニカルペーパー WAKE MODEL FOR HELICOPTER ROTORS IN HIGH SPEED FLIGHT Johnson, Wayne R. National Aeronautics and Space Administration
4 テクニカルペーパー Self-Scheduling Parallel Methods for Multiple Serial Codes with Application to WOPWOP Long, Lyle N., Brentner, Kenneth S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー CORRELATION OF HELICOPTER IMPULSIVE NOISE FROM BLADE-VORTEX INTERACTION WITH ROTOR MEAN INFLOW Connor, A. B. National Aeronautics and Space Administration
5 テクニカルペーパー Airframe noise prediction with installed landing gear for a complete aircraft Lopes, Leonard V., Brentner, Kenneth S., Morris, Philip J. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー A supersonically moving Kirchhoff surface method for delocalized high speed rotor noise prediction Francescantonio, Paolo di American Institute of Aeronautics and Astronautics
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