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Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4

By Larson, Terry J.

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Book Id: WPLBN0002208015
Format Type: PDF eBook :
File Size: 1.5 MB
Reproduction Date: 2012
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Title: Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4  
Author: Larson, Terry J.
Volume:
Language: English
Subject: BOUNDARY LAYER CONTROL, FLIGHT SIMULATION, LEADING EDGES
Collections: NASA Publication Collection
Historic
Publication Date:
1990
Publisher:

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J, L. T., M., I, S. P., & R, M. T. (1990). Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4. Retrieved from http://www.netlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Flush pressure orifices installed on the nose section of a 1/7-scale model of the F-14 airplane were evaluated for use as a flush airdata sy

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; FLIGHT SIMULATION; LEADING EDGES; LAMINAR FLOW; FLIGHT TESTS; C-140 AIRCRAFT; PERFORATION; SUCTION; ACTIVE CONTROL; AIRCRAFT CONTROL; AIRLINE OPERATIONS

 

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