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Airframe technology for energy efficient transport aircraftNASA has initiated a comprehensive Aircraft Energy Efficiency Program which is concerned with the development of approaches for reducing fuel consumption in new aircraft of the 1980-2000 time period. A review is presented of the airframe technologies selected for emphasis in the NASA program, taking into account an evaluation of their potential for reducing transport direct operating costs through fuel efficiency. Attention is given to the importance of fuel efficiency, the impact of advanced technology, advanced composite structures, the NASA composite primary structures program, advanced aerodynamics and active controls, supercritical wing geometry, active load and flutter control, and aspects of laminar flow control.
Document ID
19770045382
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leonard, R. W.
(NASA Langley Research Center Hampton, VA, United States)
Wagner, R. D.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 760929
Meeting Information
Meeting: Aerospace Engineering and Manufacturing Meeting on Cyclic structural analyses of air-cooled gas turbine blades and vanes
Location: San Diego, CA
Start Date: November 29, 1976
End Date: December 2, 1976
Sponsors: Society of Automotive Engineers
Accession Number
77A28234
Distribution Limits
Public
Copyright
Other

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