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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
20000058091
Document Type
Conference Proceedings
Authors
Baize, Daniel G.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
December 1, 1999
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.55:209691/VOL1/PT1
L-17916B
NASA/CP-1999-209691/VOL1/PT1
Meeting Information
NASA High-Speed Research Program Aerodynamic Performance Workshop(Hampton, VA)
Funding Number(s)
PROJECT: RTOP 537-07-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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