NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Technology 2003: The Fourth National Technology Transfer Conference and Exposition, volume 2Proceedings from symposia of the Technology 2003 Conference and Exposition, Dec. 7-9, 1993, Anaheim, CA, are presented. Volume 2 features papers on artificial intelligence, CAD&E, computer hardware, computer software, information management, photonics, robotics, test and measurement, video and imaging, and virtual reality/simulation.
Document ID
19940027914
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hackett, Michael (NASA Headquarters Washington, DC United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1994
Subject Category
General
Report/Patent Number
NAS 1.55:3249-VOL-2
NASA-CP-3249-VOL-2
Report Number: NAS 1.55:3249-VOL-2
Report Number: NASA-CP-3249-VOL-2
Accession Number
94N32420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19940028957WorkNASA HSR phase 1 low noise nozzle technology program overview19940028958WorkHigh speed jet noise research at NASA Lewis19940028959WorkHSCT nozzle source noise programs at Pratt and Whitney19940028960WorkHSCT noise reduction technology development at GE Aircraft Engines19940028961WorkCommunity noise sources and noise control issues19940028962WorkNASA/LaRC jet plume research19940028963WorkTheoretical aspects of supersonic jet noise19940028964WorkDesign and analysis of low boom concepts at Langley Research Center19940028965WorkHSCT design for reduced sonic boom19940028966WorkSonic boom prediction and minimization using computational fluid dynamics19940028967WorkSonic boom configuration minimization19940028968WorkSonic boom predictions using a modified Euler code19940028969WorkOverview of feasibility study on conducting overflight measurements of shaped sonic boom signatures using RPV's19940028970WorkThe NASA sponsored HSCT propulsion studies19940028971WorkA NASA Lewis comparative propulsion system assessment for the High-Speed Civil Transport19940028972WorkP and W/GE propulsion systems studies introduction19940028973WorkResults of GEAE HSCT propulsion system studies19940028974WorkP and W propulsion systems studies results/status19940028975WorkLow emissions combustor technology for high-speed civil transport engines19940028976WorkTheoretical study of thermodynamic properties and reaction rates of importance in the high-speed research program19940028977WorkHSR combustion analytical research19940028978WorkLeRC in-house experimental research19940028979WorkLean burn combustor technology at GE Aircraft Engines19940028980WorkRich burn combustor technology at Pratt and Whitney19940028957WorkNASA HSR phase 1 low noise nozzle technology program overview19940028958WorkHigh speed jet noise research at NASA Lewis19940028959WorkHSCT nozzle source noise programs at Pratt and Whitney19940028960WorkHSCT noise reduction technology development at GE Aircraft Engines19940028961WorkCommunity noise sources and noise control issues19940028962WorkNASA/LaRC jet plume research19940028963WorkTheoretical aspects of supersonic jet noise19940028964WorkDesign and analysis of low boom concepts at Langley Research Center19940028965WorkHSCT design for reduced sonic boom19940028966WorkSonic boom prediction and minimization using computational fluid dynamics19940028967WorkSonic boom configuration minimization19940028968WorkSonic boom predictions using a modified Euler code19940028969WorkOverview of feasibility study on conducting overflight measurements of shaped sonic boom signatures using RPV's19940028970WorkThe NASA sponsored HSCT propulsion studies19940028971WorkA NASA Lewis comparative propulsion system assessment for the High-Speed Civil Transport19940028972WorkP and W/GE propulsion systems studies introduction19940028973WorkResults of GEAE HSCT propulsion system studies19940028974WorkP and W propulsion systems studies results/status19940028975WorkLow emissions combustor technology for high-speed civil transport engines19940028976WorkTheoretical study of thermodynamic properties and reaction rates of importance in the high-speed research program19940028977WorkHSR combustion analytical research19940028978WorkLeRC in-house experimental research19940028979WorkLean burn combustor technology at GE Aircraft Engines19940028980WorkRich burn combustor technology at Pratt and Whitney
No Preview Available