Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
By: Lawrence C. Freudinger.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4148.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, VA
Language: eng
Format: Microform
Number of pages: 18
Subjects: Hornet (Jet fighter plane) -- Vibration.; Flutter (Aerodynamics); Research aircraft -- Vibration.; Angle of attack.; Clearances.; F-18 aircraft.; Flutter.; Wing tips.
Notes: Shipping list no.: 90-0470-M.

"Performing organization report no.: H-1528"--Technical rept. documentation p.

Includes bibliographical references (p. 7).

Also available via Internet from the NASA Technical Report Server web site. Address as of 7/27/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002416%5F1990002416.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

RTOP 533-02-71.