Important scaling parameters for testing model-scale helicopter rotors

Important scaling parameters for testing model-scale helicopter rotors

著者名:

Singleton, Jeffrey D. ( ARL Vehicle Technology Center, NASA Langley Research Center )
Yeager, William T., Jr. ( ARL Vehicle Technology Center, NASA Langley Research Center )

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA Advanced Measurement and Ground Testing Technology Conference

シリーズ巻号:

1998

発行年:

1998

通号:

98-2881

ペーパー番号:

98-2881

開始ページ:

1

終了ページ:

11

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050853
シリーズID:	PA00000145
会議名:	AIAA Advanced measurement and Ground Testing Technology Conference
回次:	20th
会議開催地:	Albuquerque, NM
会議開催年:	1998.06.15-1998.06.18
論文注記:	20th AIAA Advanced Measurement and Ground Testing Technology Conference, June 15-18, 1998/Albuquerque, NM

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1 テクニカルペーパー Perfomance Data From a Wind-Tunnel Test of Two Main-Rotor Blade Designs for Utility-Class Helicopter Singleton,Jeffrey D., Yeager, William T.,Jr., Wilbur, Matthew L. National Aeronautics and Space Adminstration	7 テクニカルペーパー WIND-TUNNEL EVALUATION OF AN ADVANCED MAIN-ROTOR BLADE DESIGN FOR A UTILITY-CLASS HELICOPTER Yeager,Jr. William T. et al. National Aeronautics and Space Administration
2 テクニカルペーパー Performance and Vibratory Loads Data From a Wind-Tunnel Test of a Model Helicopter Main-Rotor Blade With a Paddle-Type Tip Yeager, William T., Jr., Noonan, Kevin W., Singleton, Jeffrey D., Wilbur, Matthew L., Mirick, Paul H. National Aeronautics and Space Adminstration	8 テクニカルペーパー Ornicopter Yaw Control: Testing a Single Rotor Helicopter Without Reaction Torque D. van Gerwen, T. van Holten, M. Heiligers American Institute of Aeronautics and Astronautics
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4 テクニカルペーパー Wind-Tunnel Evaluation of the Effect of Blade Nonstructural Mass Distribution on Helicopter Fixed-System Loads Wilbur, Matthew L., Yeager, William T., Jr., Singleton, Jeffrey D., Mirick, Paul H., Wilkie, W. Keats National Aeronautics and Space Adminstration	10 テクニカルペーパー Analysis and testing of Mach scaled rotor model with piezoelectric bender actuated trailing-edge flaps for helicopter vibration control Koratkar, Nikhil A., Chopra, Inderjit American Institute of Aeronautics and Astronautics
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