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A feasibility study for advanced technology integration for general aviationAn investigation was conducted to identify candidate technologies and specific developments which offer greatest promise for improving safety, fuel efficiency, performance, and utility of general aviation airplanes. Interviews were conducted with general aviation airframe and systems manufacturers and NASA research centers. The following technologies were evaluated for use in airplane design tradeoff studies conducted during the study: avionics, aerodynamics, configurations, structures, flight controls, and propulsion. Based on industry interviews and design tradeoff studies, several recommendations were made for further high payoff research. The most attractive technologies for use by the general aviation industry appear to be advanced engines, composite materials, natural laminar flow airfoils, and advanced integrated avionics systems. The integration of these technologies in airplane design can yield significant increases in speeds, ranges, and payloads over present aircraft with 40 percent to 50 percent reductions in fuel used.
Document ID
19810007459
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kohlman, D. L.
(Kansas Univ. Lawrence, KS, United States)
Matsuyama, G. T.
(Kansas Univ. Lawrence, KS, United States)
Hawley, K. E.
(Kansas Univ. Lawrence, KS, United States)
Meredith, P. T.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aeronautics (General)
Report/Patent Number
KU-FRL-414-1
NASA-CR-159381
Accession Number
81N15974
Funding Number(s)
PROJECT: RTOP 530-01-13-01
CONTRACT_GRANT: NAS1-15770
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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