Overview of airframe technology in the NASA High-Speed Research ProgramNASA's Phase I High-Speed Research Program has been established to develop solutions for critical environmental issues confronting the next-generation U.S. SST, or High-Speed Civil Transport (HSCT). Attention is presently given to the ways in which HSCT environmental acceptability is affected by such airframe-technology features as laminar flow control, advanced high-lift systems for TO&L, and contour tailoring for sonic-boom minimization. The reduction of sonic booms is economically critical to the HSCT, in that it will permit overland flight at supersonic speeds and therefore maximize the reduction in long-range flight times.
Document ID
19910069402
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitehead, Allen H., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1991
Subject Category
Aeronautics (General)
Report/Patent Number
AIAA PAPER 91-3100Report Number: AIAA PAPER 91-3100