NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Flight Studies of Problems Pertinent to High-Speed Operation of Jet TransportsA flight investigation was made to assess the potential operational problems of jet transports in the transonic cruise range. In this study a large multiengine jet airplane having geometric characteristics fairly representative of the jet transport was used; however, in order to ensure general applicability of the results, the aerodynamic characteristics of the test airplane were varied to simulate a variety of jet- transport airplanes. Some of the specific areas investigated include: (1) an overall evaluation of longitudinal stability and control characteristics at transonic speeds, with an assessment of pitch-up characteristics, (2) the effect of buffeting on airplane operational speeds and maneuvering, (3) the desirable lateral-directional damping characteristics, (4) the desirable lateral-control characteristics, (5) an assessment of over-speed and speed-spread requirements, including the upset maneuver, and (6) an assessment of techniques and airplane characteristics for rapid descent and slow-down. The results presented include pilots' evaluation of the various problem areas and specific recommendations for possible improvement of jet-transport operations in the cruising speed range.
Document ID
19980228311
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Butchart, Stanley P.
(NASA Dryden Flight Research Facility Edwards, CA United States)
Fischel, Jack
(NASA Dryden Flight Research Facility Edwards, CA United States)
Tremant, Robert A.
(NASA Dryden Flight Research Facility Edwards, CA United States)
Robinson, Glenn H.
(NASA Dryden Flight Research Facility Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1959
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-MEMO-3-2-59H
Report Number: NASA-MEMO-3-2-59H
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available