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1997 NASA High-Speed Research Program Aerodynamic Performance WorkshopThe High-Speed Research Program and NASA Langley Research Center sponsored the NASA High-Speed Research Program Aerodynamic Performance Workshop on February 25-28, 1997. The workshop was designed to bring together NASA and industry High-Speed Civil Transport (HSCT) Aerodynamic Performance technology development participants in area of Configuration Aerodynamics (transonic and supersonic cruise drag prediction and minimization), High-Lift, Flight Controls, Supersonic Laminar Flow Control, and Sonic Boom Prediction. The workshop objectives were to (1) report the progress and status of HSCT aerodynamic performance technology development; (2) disseminate this technology within the appropriate technical communities; and (3) promote synergy among the scientist and engineers working HSCT aerodynamics. In particular, single- and multi-point optimized HSCT configurations, HSCT high-lift system performance predictions, and HSCT Motion Simulator results were presented along with executive summaries for all the Aerodynamic Performance technology areas.
Document ID
Acquisition Source
Langley Research Center
Document Type
Conference Proceedings
Baize, Daniel G.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Subject Category
Report/Patent Number
NAS 1.55:209691/VOL1/PT1
Meeting Information
Meeting: NASA High-Speed Research Program Aerodynamic Performance Workshop
Location: Hampton, VA
Country: United States
Start Date: February 25, 1997
End Date: February 28, 1997
Funding Number(s)
PROJECT: RTOP 537-07-00
Distribution Limits
Work of the US Gov. Public Use Permitted.
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