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Study of the integration of wind tunnel and computational methods for aerodynamic configurations

By Browne, Lindsey E.

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Book Id: WPLBN0002207922
Format Type: PDF eBook :
File Size: 1.8 MB
Reproduction Date: 2012
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Title: Study of the integration of wind tunnel and computational methods for aerodynamic configurations  
Author: Browne, Lindsey E.
Volume:
Language: English
Subject: BOUNDARY LAYER CONTROL, FLOW VISUALIZATION, F-14 AIRCRAFT
Collections: NASA Publication Collection
Historic
Publication Date:
1989
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E, B. L., & L, A. D. (1989). Study of the integration of wind tunnel and computational methods for aerodynamic configurations. Retrieved from http://www.ebooklibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; A study was conducted to determine the effectiveness of using a low-order panel code to estimate wind tunnel wall corrections. The correctio

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: BOUNDARY LAYER CONTROL; FLOW VISUALIZATION; F-14 AIRCRAFT; BOUNDARY LAYER TRANSITION; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; FLIGHT TESTS; LAMINAR FLOW; VARIABLE SWEEP WINGS; BOUNDARY LAYER STABILITY; DRAG REDUCTION; FLIGHT ENVELOPES

 

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