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Aerodynamic Characteristics of Several Current Helicopter Tail Boom Cross Sections Including the Effect of Spoilers [microform]

John C. Wilson and Henry L. Kelley
Format
Book; Government Document; Microform
Published
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, distributor], 1986.
Language
English
Series
NASA Technical Paper
AVSCOM Technical Report
SuDoc Number
NAS 1.60:2506
Description
71 p. : ill. ; 28 cm.
Notes
  • Distributed to depository libraries in microfiche.
  • "January 1986"--Cover.
  • STAR Subject category 02.
  • Includes bibliographical references (p. 6).
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 1 microfiche : negative.
Series Statement
NASA technical paper 2506
AVSCOM technical report ; 85-B-3
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers h| [microform] / c| John C. Wilson and Henry L. Kelley.
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    a| Includes bibliographical references (p. 6).
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    a| Helicopters x| Aerodynamics.
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    a| Helicopter tail rotors. 2| nasat
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    a| Tail assemblies. 2| nasat
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