X-21A research aircraft is designed to demonstrate practicality of design, manufacture, operation, and maintenance of Laminar Flow Control aircraft and to acquire data for direct application to future aircraft systems; laminar flow control principle and concept of pumping system to remove boundary layer air from wing surfaces of Laminar Flow Control aircraft; pumping system requirements and design characteristics for future applications; system selection, and system operation; pumping design and development.
Air pumping system for laminar flow control aircraft
SAE -- Paper
SAE Meeting ; 1963
1963
13 pages
Aufsatz (Konferenz)
Englisch
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Air Pumping System for a Laminar Flow Control Aircraft
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