Static performance of six innovative thrust reverser concepts for subsonic transport applications
Subtitle: summary of the NASA Langley Innovative Thrust Reverser Test Program
By: Scott C. Asbury and Jeffrey A. Yetter.
Contributors: Yetter, Jeffrey A.; Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2000-210300.; NASA technical memorandum -- 210300.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2000
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Format: Microform
Subjects: Subsonic speed.; Thrust reversal.; Turbofans.; Aircraft brakes.; Brakes (For arresting motion); Aeronautical engineering.; Aircraft design.; Performance tests.
Other titles: Summary of the NASA Langley Innovative Thrust Reverser Test Program.
Notes: Shipping list no.: 2002-0043-M.

Also available via Internet from the NASA web site. Address as of 9/30/02: http://techreports.larc.nasa.gov/ltrs/PDF/2000/tm/NASA-2000-tm210300.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000?] 4 microfiches.