NDLI: Transonic airframe propulsion integration

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Transonic airframe propulsion integration

Content Provider	NASA Technical Reports Server (NTRS)
Author	Sanders, Bobby W. Coltrin, Robert E. Bencze, Daniel P.
Copyright Year	1992
Description	This chart shows the time line for HSR propulsion/airframe integration program. HSR Phase 1 efforts are underway in both propulsion and aerodynamics. The propulsion efforts focus on cycles, inlets combustors and nozzles that will be required to reduce nitrogen oxide (NOX) at cruise and noise at takeoff and landing to acceptable levels. The aerodynamic efforts concentrate on concepts that will reduce sonic booms and increase the lift/drag (L/D) ratio for the aircraft. The Phase 2 critical propulsion component technology program will focus on large scale demonstrators of the inlet, fan, combustor, and nozzle. The hardware developed here will feed into the propulsion system program which will demonstrate overall system technology readiness, particularly in the takeoff and supersonic cruise speed ranges. The Phase 2 aerodynamic performance and vehicle integration program will provide a validated data base for advanced airframe/control/integration concepts over the full HSR speed range. The results of this program will also feed into the propulsion system demonstration program, particularly in the critical transonic arena.
File Size	811954
Page Count	22
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19940029001
Archival Resource Key	ark:/13960/t3518x828
Language	English
Publisher Date	1992-04-01
Access Restriction	Open
Subject Keyword	Aircraft Propulsion And Power Airframes Technology Assessment Engine Airframe Integration Inlet Nozzles Sonic Booms Combustion Chambers Aerodynamic Characteristics Systems Integration Propulsion System Configurations Data Bases Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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