The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system /

Bibliographic Details
Main Author:	Whitmore, Stephen A.
Corporate Authors:	Dryden Flight Research Facility, AIAA Aerospace Sciences Meeting
Other Authors:	Moes, Timothy R.
Format:	Government Document Conference Proceeding Book
Language:	English
Published:	Edwards, Calif. : NASA Ames Resarch Center, Dryden Flight Research Facility ; 1991.
Series:	NASA technical memorandum ; 101736.
Subjects:	Pressure transducers. Acoustics. Angle of attack. Design analysis. Flight conditions. Pressure effects. Pressure sensors. Research vehicles. Signal processing. Transmission lines.
Online Access:	https://purl.fdlp.gov/GPO/LPS60255

Description
Item Description:	"February 1991." Distributed to depository libraries in microfiche. Prepared as AIAA 91-0671 for presentation at the AIAA 29th Aerospace Sciences Meeting, Reno, Nevada, January 7-10, 1991. Microform.
Physical Description:	23 pages : illustrations, charts ; 28 cm. Also available via Internet from the NTRS web site. Address as of 5/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910007747%5F1991007747.pdf; current access is available via PURL.
Bibliography:	Includes bibliographical references (page 11).