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Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing

By Mirick, Paul H.

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Book Id: WPLBN0002208355
Format Type: PDF eBook :
File Size: 1.5 MB
Reproduction Date: 2012

Title: Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing  
Author: Mirick, Paul H.
Volume:
Language: English
Subject: CORRELATION, LIGHT SCATTERING, CRYOGENICS
Collections: NASA Publication Collection
Historic
Publication Date:
1990
Publisher:

Citation

APA MLA Chicago

H, M. P., T., J, Y. W., & H, H. M. (1990). Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Retrieved from http://kindle.worldlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; A survey was conducted of the flow field produced by the Airstream Oscillator System (AOS) in the Langley Transonic Dynamics Tunnel (TDT). T

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: CORRELATION; LIGHT SCATTERING; CRYOGENICS; TRANSONIC SPEED; LIQUID SURFACES; MOMENTUM TRANSFER; JET FLOW; LIQUID NITROGEN; MULTIPHASE FLOW; NITROGEN; ATOMIZERS; COMBUSTION CHAMBERS; DROP SIZE

 

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