Modification of the Ames 40-by 80-Foot Wind Tunnel for Component Acoustic Testing for the Second Generation Supersonic Transport | 東京工業大学附属図書館文献データベース

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Modification of the Ames 40-by 80-Foot Wind Tunnel for Component Acoustic Testing for the Second Generation Supersonic Transport

著者名:

Schmitz, F.H. ( Ames Research Center )
Allmen, J.R.
Soderman, P.T.

掲載資料名:

NASA Technical Reports

発行年:

1994

通号:

N95-13642

ペーパー番号:

N95-13642

開始ページ:

1

終了ページ:

41

総ページ数:

41

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:

ZA00001431

類似資料:

1 テクニカルペーパー Design of deep acoustic lining for the 40- by 80- Foot Wind Tunnel test section Soderman, Paul T., Schmitz, Fredric H., Allen, Christopher S., Jaeger, Stephen M., Sacco, Joe N., Hayes, Julie A. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Airframe Noise Study of a CRJ-700 Aircraft Model in the NASA Ames 7-by 10-Foot Wind Tunnel No. 1 Soderman, P., Kafyeke, F., Burnside, N., Chandrasekharan, R., Jaeger, S., Boudreau, J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー SOURCES AND LEVELS OF BACKGROUND NOISE IN THE NASA AMES 40- BY 80-FOOT WIND TUNNEL Status Report Soderman, Paul T. National Aeronautics and Space Administration	8 テクニカルペーパー FLOW DIRECTION MEASUREMENT CRITERIA AND TECHNIQUES PLANNED FOR THE 40- BY 80- 80- X 120-FOOT WIND TUNNEL Zell., P.T. National Aeronautics and Space Administration
3 テクニカルペーパー The Design of Test-Section Inserts for Higher Speed Aeroacoustic Testing in the Ames 80- by 120-Foot Wind Tunnel Soderman, Paul T., Olson, Larry E. National Aeronautics and Space Adminstration	9 テクニカルペーパー Shake Test Results of the MDHC Test Stand in the 40- by 80-Foot Wind Tunnel Lau, Benton H., Peterson, Randall National Aeronautics and Space Adminstration
4 テクニカルペーパー Measurements of 26%-Scale 777 Airframe Noise in the NASA Ames 40- by 80 Foot Wind Tunnel Horne, W., James, K., Arledge, T., Soderman, P., Burnside, N., Jaeger, S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー ONE-FIFTIETH SCALE MODEL STUDIES OF 40-BY 80-FOOT AND 80-BY 120-FOOT WIND TUNNEL COMPLEX AT NASA AMES RESEARCH Schmidt, G.I. National Aeronautics and Space Administration
5 テクニカルペーパー Large-Scale Aeroacousitic Research Feasibiligy and Conceptual Design of Test-Section Inserts for the Ames 80-by 120-Foot Wind Tunnel Soderman, Paul T., Olson, Larry E. National Aeronautics and Space Adminstration	11 テクニカルペーパー Prediction of the Flow-Field Interference Induced by the Long-Range Laser Velocimeter in the Ames 40- by 80-Foot nad the 80- by 120-Foot Wind Tunnels Reinath, Michael S., Ross, James C. National Aeronautics and Space Administration
6 テクニカルペーパー Aerodynamic Flow Quality and Acoustic Characteristics of the 40-by 80-Foot Test Section Circuit of the National Full-Scale Aerodynamic Complex Olson,Lawrence E., Zell,Peter T., Soderman,Paul T., Falarski,Michael D., Corsiglia,Victor R., Edenborough,H.Kipling Society of Automotive Engineers	12 テクニカルペーパー PERFORMANCE AND TEST SECTION FLOW CHARACTERISTICS OF THE NATIONAL FULL-SCALE AERODYNAMICS COMPLEX 40-BY 80-FOOT WIND TUNNEL Zell, Peter T. et al. National Aeronautics and Space Administration

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