Item Details

Results of Aerothermodynamic and Boundary Layer Transition Testing of 0.0362-Scale X-38 (Rev 3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel [microform]

Scott A. Berry ... [et al.]
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 Memorandum
SuDoc Number
NAS 1.15:112857
Description
1 v.
Notes
Shipping list no.: 99-0055-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches.
Series Statement
NASA technical memorandum 112857
Technical Details
  • Access in Virgo Classic

  • LEADER 01524nam a22003857a 4500
    001 u2920546
    003 SIRSI
    005 19990503162820.0
    008 990503s1997 vau b f000 0 eng d
    035
      
      
    a| (Sirsi) ocm41291947
    035
      
      
    a| (OCoLC)41291947
    037
      
      
    a| 19970031678 b| NASA
    040
      
      
    a| GPO c| GPO d| DLC d| MvI
    049
      
      
    a| VAMM
    074
      
      
    a| 0830-D (MF)
    086
    0
      
    a| NAS 1.15:112857
    245
    0
    0
    a| Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel h| [microform] / c| Scott A. Berry ... [et al.].
    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 memorandum v| 112857
    500
      
      
    a| Shipping list no.: 99-0055-M.
    533
      
      
    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1997] e| 2 microfiches.
    596
      
      
    a| 2
    650
      
    7
    a| Boundary layer transition. 2| nasat
    650
      
    7
    a| Aerodynamic heating. 2| nasat
    650
      
    7
    a| Wind tunnel tests. 2| nasat
    650
      
    7
    a| Angle of attack. 2| nasat
    650
      
    7
    a| Reynolds number. 2| nasat
    650
      
    7
    a| Aerothermodynamics. 2| nasat
    650
      
    7
    a| Flow visualization. 2| nasat
    700
    1
      
    a| Berry, Scott A.
    710
    2
      
    a| Langley Research Center.
    999
      
      
    a| NAS 1.15:112857 w| SUDOC i| 2920546-1001 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.