The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system
By: Stephen A. Whitmore, Timothy R. Moes.
Contributors: Moes, Timothy R.; Dryden Flight Research Facility.; AIAA Aerospace Sciences Meeting (29th : 1991 : Reno, Nevada)
Series: NASA technical memorandum -- 101736.
Publisher: NASA Ames Resarch Center, Dryden Flight Research Facility; National Technical Information Service, distributor]
Published: 1991
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 23
Subjects: Pressure transducers.; Acoustics.; Angle of attack.; Design analysis.; Flight conditions.; Pressure effects.; Pressure sensors.; Research vehicles.; Signal processing.; Transmission lines.
Notes: "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.

Includes bibliographical references (p. 11).

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche.