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NASA Technical Reports Server (NTRS) 19930002033: Overview of super...
by NASA Technical Reports Server (NTRS)
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NASA is directing research to develop technology for a
high-speed civil transport. Supersonic laminar flow
control has been identified as a program element, since
it offers significant drag-reduction benefits and is one
of the more promising technologies for producing an
economically viable aircraft design. NASA is using two
prototype F-16XL aircraft to research supersonic laminar
flow control. The F-16XL planform is similar to design
planforms of high-speed civil transports. The planform
makes the aircraft ideally suited for developing
technology pertinent to high-speed transports. The
supersonic laminar flow control research programs for
both aircraft are described. Some general results of the
ship-1 program demonstrate that significant laminar flow
was obtained using laminar flow control on a highly swept
wing at supersonic speeds.
Date Published: 2016-09-30 13:13:52
Identifier: NASA_NTRS_Archive_19930002033
Item Size: 18965811
Language: english
Media Type: texts
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