NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
HSCT high-lift technology requirementsThe viewgraphs and discussion of high lift needs and related aerodynamic goals established in system studies are described. The goals are presented for the takeoff, approach, and subsonic climb and cruise modes. The status of the related high lift databases and available design and analysis methods are described. Various high lift research and technology areas for future work including innovative concepts verification, flap design, computational fluid dynamics (CFD) calibration and application, high Reynolds number testing, subsonic/transonic flap optimization, and flight testing are described.
Document ID
19940029017
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Antani, D. L.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Morgenstern, J. M.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Publication Information
Publication: NASA. Langley Research Center, First Annual High-Speed Research Workshop, Part 4
Subject Category
Aerodynamics
Accession Number
94N33523
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available