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Further Investigation of a Finite Difference Procedure for Analyzing the Transonic Flow About Harmonically Oscillating Airfoils and Wings

W. H. Wetherill ... [et al.] ; prepared for Langley Research Center under contract NAS1-15128
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:3195
Description
79 p. : ill. ; 27 cm.
Notes
  • "May 1980"--Cover.
  • STAR category no. 02.
  • Includes bibliographical references.
Series Statement
NASA contractor report 3195
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Further investigation of a finite difference procedure for analyzing the transonic flow about harmonically oscillating airfoils and wings / c| W. H. Wetherill ... [et al.] ; prepared for Langley Research Center under contract NAS1-15128.
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    a| Aerodynamics, Transonic.
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