Steady and Periodic Pressure Measurements on a Generic Helicopter Fuselage Model in the Presence of a Rotor
Raymond E. Mineck
Jan 2000 · NASA
1.0star
1 review
Ebook
188
Pages
About this ebook
Helicopter airframes are subjected to periodic air-loads due principally to the rotating main rotor blades. The periodic air loads impact the noise and vibration within the passenger cabin as well as the fatigue life of the airframe. Computational techniques have been and are being developed to predict these periodic airframe air loads. Periodic pressure measurements are needed on simple configurations for validation of the computational techniques. Few experimental data sets are available in the open literature. Available results are typically limited to a few measurement stations and test conditions. The purpose of this investigation is to obtain steady and periodic pressure distributions on a generic helicopter configuration suitable for CFD validation studies.
Ratings and reviews
1.0
1 review
Rate this ebook
Tell us what you think.
Reading information
Smartphones and tablets
Install the Google Play Books app for Android and iPad/iPhone. It syncs automatically with your account and allows you to read online or offline wherever you are.
Laptops and computers
You can listen to audiobooks purchased on Google Play using your computer's web browser.
eReaders and other devices
To read on e-ink devices like Kobo eReaders, you'll need to download a file and transfer it to your device. Follow the detailed Help Center instructions to transfer the files to supported eReaders.
