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Airfoil Modification Effects on Subsonic and Transonic Pressure Distributions and Performance for the EA-6B Airplane [microform]

Dennis O. Allision and William G. Sewall
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service (NTIS) [distributor, 1995]
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:3516
Notes
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0744-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Series Statement
NASA technical paper 3516
Technical Details
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  • Staff View

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    a| Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane h| [microform] / c| Dennis O. Allision and William G. Sewall.
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    a| 2
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    a| Aircraft models. 2| nasat
    650
      
    7
    a| Airfoils. 2| nasat
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    7
    a| Leading edges. 2| nasat
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    7
    a| Maneuverability. 2| nasat
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    a| Pressure distribution. 2| nasat
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    a| Subsonic speed. 2| nasat
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    a| Trailing edges. 2| nasat
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    7
    a| Transonic speed. 2| nasat
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    a| Wind tunnel tests. 2| nasat
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    a| Wing-fuselage stores. 2| nasat
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    a| Sewall, William G.
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