NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
High speed civil transport aerodynamic optimizationThis is a report of work in support of the Computational Aerosciences (CAS) element of the Federal HPCC program. Specifically, CFD and aerodynamic optimization are being performed on parallel computers. The long-range goal of this work is to facilitate teraflops-rate multidisciplinary optimization of aerospace vehicles. This year's work is targeted for application to the High Speed Civil Transport (HSCT), one of four CAS grand challenges identified in the HPCC FY 1995 Blue Book. This vehicle is to be a passenger aircraft, with the promise of cutting overseas flight time by more than half. To meet fuel economy, operational costs, environmental impact, noise production, and range requirements, improved design tools are required, and these tools must eventually integrate optimization, external aerodynamics, propulsion, structures, heat transfer, controls, and perhaps other disciplines. The fundamental goal of this project is to contribute to improved design tools for U.S. industry, and thus to the nation's economic competitiveness.
Document ID
19950005976
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ryan, James S.
(MCAT Inst. San Jose, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:196960
NASA-CR-196960
Report Number: NAS 1.26:196960
Report Number: NASA-CR-196960
Accession Number
95N12389
Funding Number(s)
CONTRACT_GRANT: NCC2-796
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available