The NASA Supersonic Laminar Flow Control (SLFC) program encompasses the development of refined CFD methods and boundary layer stability codes for the highly 3D supersonic flow conditions encountered by the F-16XL technology demonstration aircraft and the prospective High Speed Civil Transport (HSCT). While the F-16XL-1 aircraft continues to gather SLFC data, work is under way on the F-16XL-2 aircraft: which will furnish attach-line design criteria, code-calibration data, and an improved understanding of the flowfield over a wing that will add confidence to the design of HSCTs' boundary layer-controlling air-suction panels.
Application of laminar flow control to the High Speed Civil Transport - The NASA Supersonic Laminar Flow Control Program
1991-09-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
SAE Technical Papers | 1991
|Laminar Design for Supersonic Civil Transport
British Library Conference Proceedings | 2001
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