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The design of high-performance glidersA high-performance glider is defined as a glider which has been designed to carry the pilot in a minimum of time a given distance, taking into account conditions which are as conveniently as possible. The present investigation has the objective to show approaches for enhancing the cross-country flight cruising speed, giving attention to the difficulties which the design engineer will have to overcome. The characteristics of the cross-country flight and their relation to the cruising speed are discussed, and a description is provided of mathematical expressions concerning the cruising speed, the sinking speed, and the optimum gliding speed. The effect of aspect ratio and wing loading on the cruising speed is illustrated with the aid of a graph. Trends in glider development are explored, taking into consideration the design of laminar profiles, the reduction of profile-related drag by plain flaps, and the variation of wing loading during the flight. A number of suggestions are made for obtaining gliders with improved performance.
Document ID
19850015439
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mueller, B.
(NASA Headquarters Washington, DC United States)
Heuermann, V.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
DGLR-T-83-01
NASA-TM-77772
NAS 1.15:77772
Report Number: DGLR-T-83-01
Report Number: NASA-TM-77772
Report Number: NAS 1.15:77772
Accession Number
85N23750
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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