Item Details

Print View

High-Resolution Shock Capturing Scheme for High Mach Number Internal Flow [microform]

Seokkwan Yoon and Antony Jameson
Format
Book; Government Document; Microform
Published
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
Language
English
Variant Title
High resolution shock capturing scheme for high Mach number internal flow
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:179523
Description
1 v.
Notes
Distributed to depository libraries in microfiche.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] 1 microfiche.
Series Statement
NASA contractor report 179523
Technical Details
  • Access in Virgo Classic
  • Staff View

    LEADER 01531nam a22003857a 4500
    001 u2502519
    003 SIRSI
    008 951024s1986 dcu b f000 0 eng d
    035
      
      
    a| (Sirsi) o33351281
    035
      
      
    a| (OCoLC)33351281
    035
      
      
    a| (GPO)96060988
    037
      
      
    a| N 87-16804 b| NASA
    040
      
      
    a| GPO c| GPO d| DLC d| MvI
    049
      
      
    a| VAMM
    074
      
      
    a| 0830-H-14 (MF)
    086
    0
      
    a| NAS 1.26:179523
    100
    1
      
    a| Yoon, Seokkwan.
    245
    1
    0
    a| High-resolution shock capturing scheme for high Mach number internal flow h| [microform] / c| Seokkwan Yoon and Antony Jameson.
    246
    2
      
    a| High resolution shock capturing scheme for high Mach number internal flow
    260
      
      
    a| [Washington, D.C.] : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| National Technical Information Service, distributor, c| 1986]
    300
      
      
    a| 1 v.
    440
      
    0
    a| NASA contractor report v| 179523.
    500
      
      
    a| Distributed to depository libraries in microfiche.
    533
      
      
    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1987] e| 1 microfiche.
    596
      
      
    a| 2
    650
      
    7
    a| Computational fluid dynamics. 2| nasat
    650
      
    7
    a| High resolution. 2| nasat
    650
      
    7
    a| Hypersonic flow. 2| nasat
    650
      
    7
    a| Mach number. 2| nasat
    650
      
    7
    a| Shock waves. 2| nasat
    700
    1
      
    a| Jameson, Antony, d| 1934-
    710
    1
      
    a| United States. b| National Aeronautics and Space Administration.
    999
      
      
    a| NAS 1.26:179523 w| SUDOC i| 2502519-1001 l| 3EAST m| ALDERMAN t| MICROFICHE
▾See more
▴See less

Availability

Google Preview

Google Books Preview
Library Location Map Availability Call Number
Alderman 3rd Floor East Reading Room N/A Available Non-Circ.