Perfomance Data From a Wind-Tunnel Test of Two Main-Rotor Blade Designs for Utility-Class Helicopter
- 著者名:
- Singleton,Jeffrey D. ( Langley Research Center )
- Yeager, William T.,Jr.
- Wilbur, Matthew L.
- 掲載資料名:
- NASA Technical Reports
- 発行年:
- 1990
- 号:
- NASA-TM-4183
- 通号:
- H1/05 0270155
- パート:
- NAS 1.15:4183
- ペーパー番号:
- N90-20974
- 開始ページ:
- 1
- 終了ページ:
- 82
- 総ページ数:
- 82
- 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
類似資料:
National Aeronautics and Space Adminstration |
7
テクニカルペーパー
Application of a PC Based, Real-Time, Data-Acquisition System in Rotorcraft Wind-Tunnel Testing
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
3
テクニカルペーパー
WIND-TUNNEL EVALUATION OF AN ADVANCED MAIN-ROTOR BLADE DESIGN FOR A UTILITY-CLASS HELICOPTER
National Aeronautics and Space Administration |
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
10
テクニカルペーパー
ROTOR PERFORMANCE CHARACTERISTICS FROM AN AEROACOUSTIC HELICOPTER WING-TUNNEL TEST PROGRAM
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
6
テクニカルペーパー
Wind-Tunnel Survey of an Oscillating Flow Field for Application to Model Helicopter Rotor Testing
National Aeronautics and Space Adminstration |
12
テクニカルペーパー
A WIND TUNNEL TEST OF 22% SCALE MODEL OF A WINDMILL WITH A TWO-BLADED ROTOR OF 14m DIAMETER FOR FIELD TEST
National Aeronautics and Space Administration |