Current activities on the High Speed Civil Transport (HSCT) at Douglas are focussed on baseline vehicle development at Mach 1.6 and 2.4. Parallel design activities incorporating the latest technologies in structures/materials, propulsion/noise, and aerodynamics are also being conducted and incorporated into the baseline to establish performance, economic viability, and environmental compliance. Studies are also being conducted to establish the feasibility of incorporating laminar flow control and minimized sonic boom concepts into the baseline. A decision point on these last two technologies is targeted prior to the start of the NASA HSR Phase 2 Program in 1993.
Douglas Aircraft HSCT Status and Future Research Needs
1992
24 pages
Report
Keine Angabe
Englisch
Aerodynamics , Jet & Gas Turbine Engines , Air Pollution & Control , Noise Pollution & Control , Aerodynamic configurations , Aircraft design , Aircraft engines , Douglas aircraft , Environment effects , Noise reduction , Passenger aircraft , Supersonic transports , Aircraft structures , Boundary layer control , Jet aircraft noise , Mach number , Ozone depletion , Sonic booms , Supersonic speed
Douglas Aircraft HSCT status and future research needs
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