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Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 50̊ [microform]

Scott P. Fears, Holly M. Ross, and Thomas M. Moul
Format
Book; Government Document; Microform
Published
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Language
English
Variant Title
Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:4640
Description
1 v.
Notes
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 96-0058-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 2 microfiches.
Series Statement
NASA technical memorandum 4640
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊
    260
      
      
    a| [Washington, DC : b| National Aeronautics and Space Administration ; a| Springfield, Va. : b| National Technical Information Service, distributor, c| 1995]
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    a| 1 v.
    440
      
    0
    a| NASA technical memorandum v| 4640
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    a| Distributed to depository libraries in microfiche.
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    a| Shipping list no.: 96-0058-M.
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    a| Microfiche. b| [Washington, D.C. : c| National Aeronautics and Space Administration, d| 1995] e| 2 microfiches.
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    a| 2
    650
      
    7
    a| Aerodynamic stability. 2| nasat
    650
      
    7
    a| Angle of attack. 2| nasat
    650
      
    7
    a| Aspect ratio. 2| nasat
    650
      
    7
    a| Flight control. 2| nasat
    650
      
    7
    a| Flight stability tests. 2| nasat
    650
      
    7
    a| Leading edge flaps. 2| nasat
    650
      
    7
    a| Low speed. 2| nasat
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    7
    a| Planforms. 2| nasat
    650
      
    7
    a| Stabilizers (Fluid dynamics) 2| nasat
    650
      
    7
    a| Tail assemblies. 2| nasat
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    7
    a| Trailing edge flaps. 2| nasat
    650
      
    7
    a| Wind tunnel tests. 2| nasat
    650
      
    7
    a| Wing profiles. 2| nasat
    700
    1
      
    a| Moul, Thomas M.
    710
    1
      
    a| United States. b| National Aeronautics and Space Administration.
    948
      
      
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    999
      
      
    a| NAS 1.15:4640 w| SUDOC i| 2521194-1001 l| 3EAST m| ALDERMAN t| MICROFICHE
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