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Unsteady Flows in a Single-Stage Transonic Axial-Flow Fan Stator Row [microform]

Michael D. Hathaway
Format
Book; Government Document; Microform
Published
[Washington, D.C.] : National Aeronautics and Space Administration ; [St. Louis, MO] : U.S. Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
Language
English
Variant Title
Unsteady flows in a single stage transonic axial-flow fan stator row
Series
NASA Technical Memorandum
USAAVSCOM Technical Report
AVSCOM Technical Report
SuDoc Number
NAS 1.15:88929
Description
vii, 200 p. : ill. ; 28 cm.
Notes
  • Cover title.
  • Distributed to depository libraries in microfiche.
  • "December 1986."
  • Includes bibliographical references (p. 145-156).
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] 3 microfiches ; negative.
Series Statement
NASA technical memorandum 88929
USAAVSCOM technical report ; 86-C-29
AVSCOM technical report ; 86-C-29
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Unsteady flows in a single-stage transonic axial-flow fan stator row h| [microform] / c| Michael D. Hathaway.
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    a| Unsteady flows in a single stage transonic axial-flow fan stator row
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    a| [Washington, D.C.] : b| National Aeronautics and Space Administration ; a| [St. Louis, MO] : b| U.S. Army Aviation Systems Command ; a| [Springfield, Va. : b| For sale by the National Technical Information Service, c| 1986]
    300
      
      
    a| vii, 200 p. : b| ill. ; c| 28 cm.
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    a| NASA technical memorandum v| 88929
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    1
      
    a| USAAVSCOM technical report ; v| 86-C-29
    500
      
      
    a| Cover title.
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    a| Distributed to depository libraries in microfiche.
    500
      
      
    a| "December 1986."
    504
      
      
    a| Includes bibliographical references (p. 145-156).
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    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1987] e| 3 microfiches ; negative.
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    0
    a| Unsteady flow (Aerodynamics) x| Measurement.
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    0
    a| Turbomachines x| Performance.
    650
      
    7
    a| Axial flow turbines. 2| nasat
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    7
    a| Stator blades. 2| nasat
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    7
    a| Transonic flow. 2| nasat
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    7
    a| Turbocompressors. 2| nasat
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    7
    a| Turbo engines. 2| nasat
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    7
    a| Unsteady flow. 2| nasat
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    a| AVSCOM technical report ; v| 86-C-29.
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    a| United States. b| National Aeronautics and Space Administration.
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    1
      
    a| United States. b| Army Aviation Systems Command.
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    a| NAS 1.15:88929 w| SUDOC i| 2500878-1001 l| 3EAST m| ALDERMAN t| MICROFICHE
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