Unified Aeroacoustics Analysis for High speed Turboprop Aerodynamics and Noise : Volume III - Application of Theory for Blade Loading, Wakes, Noise, and Wing shielding

Unified Aeroacoustics Analysis for High speed Turboprop Aerodynamics and Noise : Volume III - Application of Theory for Blade Loading, Wakes, Noise, and Wing shielding

著者名:

Hanson, D.B. ( United technologies Corporation Hamilton Standerd Division Windsor Locks, Connecticut )
McColgan, C.J,
Ladden, R.M.
Klatte, R.J.

掲載資料名:

NASA Technical Reports

発行年:

1991

号:

NASA-CR-185193

通号:

G3/71 0013657

パート:

NAS 1.26:185193

ペーパー番号:

N91-23850

開始ページ:

1

終了ページ:

128

総ページ数:

128

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:	ZA00001427
論文注記:	NAS3-23720

類似資料:

1 テクニカルペーパー Unified Aeroacoustics Analysis for High Speed Turboprop Aerodynamics and Noise : Volime I-Development of Theory for Blade Loading, Wakes, and Noise Hanson, D.B. National Aeronautics and Space Adminstration	7 テクニカルペーパー High Speed Turboprop Aeroacoustic Study (Counterrotation) : Volume I - Model Development Whitfield, C.E., Mani, R., Gliebe, P.R. National Aeronautics and Space Adminstration
2 テクニカルペーパー Unified Aeroacoustics Analysis for High speed Turboprop Aerodynamics and Noise : Volume IV - Computer User's Manual for UAAP Turboprop Aeroacoustic Code Menthe, R.W., Mccologan, C,J., Ladden, R.M. National Aeronautics and Space Adminstration	8 テクニカルペーパー AN EXPERIMENTAL INVESTIGATION OF REDUCING ADVANCED TURBOPROP CABIN NOISE BY WING SHIELDING Dittmar, J.H. National Aeronautics and Space Administration
3 テクニカルペーパー Unified Aeroacoustics Analysis for High speed Turboprop Aerodynamics and Noise : Volume V Magliozzi, B., Hanson, D.B. National Aeronautics and Space Adminstration	9 テクニカルペーパー User's Manual for UCAP: Unified Counter-rotation Aero-acoustics Program Culver, E.M., McColgan, C.J. National Aeronautics and Space Adminstration
4 テクニカルペーパー Unified Aeroacoustics Analysis for High Speed Turboprop Aerodynamics and noise : volume II - development of Theory for wing Shielding Amiet, R.K. National Aeronautics and Space Adminstration	10 テクニカルペーパー ADVANCED TURBOPROP WING INSTALLATION EFFECTS MEASURED BY UNSTEADY BLADE PRESSURE AND NOISE Heidelberg, Laurence J. et al. National Aeronautics and Space Administration
5 テクニカルペーパー Coupled 2-Dimensional Cascade Theory for Noise and Unsteady Aerodynamics of Blade Row Interaction in Turbofans : Volume 1-Theory Development and Parametric … Hanson, Donald B. National Aeronautics and Space Adminstration	11 テクニカルペーパー Wake Geometry Effects on Rotor Blade-Vortex Interaction Noise Directivity Martin, R.M., Marcolini, Michael A., Splettstoesser, W.R., Schultz, K.-J. National Aeronautics and Space Adminstration
6 テクニカルペーパー Coupled 2-Dimensional Cascade Theory for Noise and Unsteady Aerodynamics of Blade Row Interaction in Turbofans : Volume 2-Documentation for Computer Code CUP2D Hanson, Donald B. National Aeronautics and Space Adminstration	12 テクニカルペーパー Free-to-Roll Analysis of Abrupt Wing Stall on Military Aircraft at Transonic Speeds. Owens, D.B., Capone, F.J., Hall, R.M., Brandon, J.M., Cunningham, K. American Institute of Aeronautics and Astronautics

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