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Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system: Design, calibration, and flight test evaluation

By Whitmore, Stephen A.

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Book Id: WPLBN0002207991
Format Type: PDF eBook :
File Size: 1.0 MB
Reproduction Date: 2012
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Title: Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system: Design, calibration, and flight test evaluation  
Author: Whitmore, Stephen A.
Volume:
Language: English
Subject: DYNAMIC CHARACTERISTICS, LOADS (FORCES), SPACECRAFT STRUCTURES
Collections: NASA Publication Collection
Historic
Publication Date:
1989
Publisher:

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A, W. S., J, L. T., & R, M. T. (1989). Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system: Design, calibration, and flight test evaluation. Retrieved from http://worldebooklibrary.com/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; A nonintrusive high angle-of-attack flush airdata sensing (HI-FADS) system was installed and flight-tested on the F-18 high alpha research f

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: DYNAMIC CHARACTERISTICS; LOADS (FORCES); SPACECRAFT STRUCTURES; REDUNDANCY; MANIPULATORS; OPTIMIZATION; TECHNOLOGY UTILIZATION; AEROSPACE ENGINEERING; DEGREES OF FREEDOM; KINEMATICS

 

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