Preliminary results from a subsonic high-angle-of-attack flush airdata sensing (HI-FADS) system - Design, calibration, algorithm development, and flight test evaluation-Reference-Cited by-同舟云学术

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

Published:1990-01-08 Issue: Volume: Page:
ISSN:
Container-title:28th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

WHITMORE STEPHEN¹,MOES TIMOTHY¹,LARSON TERRY²

Affiliation:

1. NASA, Flight Research Center,Edwards, CA

2. Analytical Mechanics Associates, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-232

Reference17 articles.

1. Larson,TerryJ.,andSicmcrs,Paul M.,IIJ,SubsonicInvesligation of anAll F'lushOri/icesAirduin Sysletn,NASA TP-1643, 1980.

2. 5Richardson,Norman R., and Pcarson,Albiii O.,Wind-Tunnel Calibrations of a Combined Pilor-Slalic Tube, Vane-lype Flow-Direclion 7ransmiiter. mid Slugnation-Temperalure Element a1Mach Numbersfrotn 0.601o 2.87, NASA TN D-122,1959.

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