The NASA High Speed Research (HSR) Program is intended to establish a technology base enabling industry development of an economically viable and environmentally acceptable second generation high speed civil transport (HSCT). The objective of the Configuration Aerodynamics task of the program is the development of aerodynamic drag reduction, stability and control, and propulsion airframe integration technologies required to support the HSCT development process. Aerodynamic design tools are being developed, evaluated, and validated through ground based experimental testing. In addition, methods for ground to flight scaling are being developed and refined.
High Reynolds Number Predictions for the Baseline Arrow Wing at Mach 2.48
1999-12-01
Conference paper
No indication
English
Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections
Online Contents | 2013
|New high Reynolds number Mach 8 capability
AIAA | 1992
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