Item Details

Invariance of Hypersonic Normal Force Coefficients With Reynolds Number and Determination of Inviscid Wave Drag From Laminar Experimental Results [microform]

Jim A. Penland and Richard Hawkins
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:3673
Description
1 v.
Notes
Shipping list no.: 1999-0723-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Series Statement
NASA technical paper 3673
Technical Details
  • Access in Virgo Classic

  • LEADER 01762nam a22004577a 4500
    001 u2933901
    003 SIRSI
    005 19991021113526.0
    008 991021s1997 vau b f000 0 eng d
    035
      
      
    a| (Sirsi) tmp97153949
    035
      
      
    a| (OCoLC)42677545
    037
      
      
    a| 19980008542 b| NASA
    040
      
      
    a| GPO c| GPO d| DLC d| MvI
    049
      
      
    a| VAMM
    074
      
      
    a| 0830-H-15 (MF)
    086
    0
      
    a| NAS 1.60:3673
    100
    1
      
    a| Penland, Jim A.
    245
    1
    0
    a| Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results h| [microform] / c| Jim A. Penland and Richard Hawkins.
    260
      
      
    a| Hampton, Va. : b| National Aeronautics and Space Administration, Langley Research Center ; a| Springfield, VA : b| National Technical Information Service, distributor, c| [1997]
    300
      
      
    a| 1 v.
    440
      
    0
    a| NASA technical paper v| 3673
    500
      
      
    a| Shipping list no.: 1999-0723-M.
    533
      
      
    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, c| 1998] e| 1 microfiche.
    596
      
      
    a| 2
    650
      
    7
    a| Hypersonic shock. 2| nasat
    650
      
    7
    a| Hypersonic boundary layer. 2| nasat
    650
      
    7
    a| Hypersonic forces. 2| nasat
    650
      
    7
    a| Turbulent boundary layer. 2| nasat
    650
      
    7
    a| Reynolds number. 2| nasat
    650
      
    7
    a| Mach number. 2| nasat
    650
      
    7
    a| Computational fluid dynamics. 2| nasat
    650
      
    7
    a| Body-wing configurations. 2| nasat
    650
      
    7
    a| Aerodynamic drag. 2| nasat
    650
      
    7
    a| Aerodynamic coefficients. 2| nasat
    700
    1
      
    a| Hawkins, Richard.
    710
    2
      
    a| Langley Research Center.
    900
      
      
    a| tmp97153949
    999
      
      
    a| NAS 1.60:3673 w| SUDOC i| X005054664 l| 3EAST m| ALDERMAN t| MICROFICHE

Availability

Google Preview

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