Item Details

A Rapid Numerical Solution to Subsonic Flow Over Planar and Axisymmetric Profiles at an Angle of Attack of 0 ̊

by Vincent R. Mascitti
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service]
Language
English
Series
NASA Technical Note
Description
31 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
  • Includes bibliographical references (p. 20).
Series Statement
NASA technical note ; NASA TN D-7410
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| A rapid numerical solution to subsonic flow over planar and axisymmetric profiles at an angle of attack of 0 ̊/ c| by Vincent R. Mascitti.
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    a| Prepared at Langley Research Center.
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    a| Includes bibliographical references (p. 20).
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    a| Mode of access: Internet.
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    a| Aerodynamics x| Computer simulation.
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