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Inflow Measurements made with a Laser Velocimeter on a Helicopter Model in Forward Flight. Volume 7: Rectangular Planform Blades at an Advance Ratio Of 0.40

By Hoad, Danny R.

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Book Id: WPLBN0002209604
Format Type: PDF eBook :
File Size: 7.8 MB
Reproduction Date: 2012

Title: Inflow Measurements made with a Laser Velocimeter on a Helicopter Model in Forward Flight. Volume 7: Rectangular Planform Blades at an Advance Ratio Of 0.40  
Author: Hoad, Danny R.
Volume:
Language: English
Subject: ADVANCED LAUNCH SYSTEM (STS), FLOW DISTRIBUTION, TIME DEPENDENCE
Collections: NASA Publication Collection
Historic
Publication Date:
1989
Publisher:

Citation

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R, H. D., W, E. J., H, S. R., & L, A. S. (1989). Inflow Measurements made with a Laser Velocimeter on a Helicopter Model in Forward Flight. Volume 7: Rectangular Planform Blades at an Advance Ratio Of 0.40. Retrieved from http://ebook2.worldlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; An experimental investigation was conducted in the 14- by 22-Foot Subsonic Tunnel at the NASA Langley Research Center to measure the inflow

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: ADVANCED LAUNCH SYSTEM (STS); FLOW DISTRIBUTION; TIME DEPENDENCE; THERMAL STRESSES; HYDROGEN OXYGEN ENGINES; SYSTEMS INTEGRATION; TRAJECTORIES; AEROTHERMODYNAMICS; BASE HEATING; LAUNCH VEHICLES; LIQUID ROCKET PROPELLANTS; PERFORMANCE PREDICTION; PROPULSION SYSTEM CONFIGURATIONS; PROPULSION SYSTEM PERFORMANCE

 

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