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Flight investigation of the roll requirements for transport airplanes in the landing approach / by Euclid C. Holleman and Bruce G. Powers.

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Format:
Book
Government document
Author/Creator:
Holleman, Euclid C., author.
Powers, Bruce G., author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Series:
NASA technical note ; D-7062.
NASA/TN ; D-7062
Language:
English
Subjects (All):
Rolling (Aerodynamics).
Airplanes--Landing.
Airplanes.
Transport planes.
Physical Description:
1 online resource (48 pages) : illustrations.
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, October 1972.
Summary:
An in-flight evaluation of transport roll characteristics in the landing approach was made with a general purpose airborne simulator. The evaluation task consisted of an instrument approach with a visual correction for a (200-foot) lateral offset. Pilot evaluations and ratings were obtained for approaches made at 140 knots and 180 knots indicated airspeed with variations of wheel characteristics, maximum roll rate, and roll time constant.
Notes:
"October 1972."
Includes bibliographical references (page 12).
Description based on online resource, PDF version; title from title page (NASA, viewed on June 1, 2021).
Other Format:
Online version: Holleman, Euclid C. Flight investigation of the roll requirements for transport airplanes in the landing approach
OCLC:
23292686

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