Item Details

Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8 Scale F-15 Airplane Model Obtained From Flight Test

Kenneth W. Iliff, Richard E. Maine, and Mary F. Shafer
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], 1976.
Language
English
Series
NASA Technical Note
Description
31 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at NASA Flight Research Center.
  • Cover title.
  • Includes bibliographical references (p. 13).
Series Statement
NASA technical note ; NASA TN D-8136
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8 scale F-15 airplane model obtained from flight test / c| Kenneth W. Iliff, Richard E. Maine, and Mary F. Shafer.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1976.
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    a| 31 p. : b| ill. ; c| 27 cm.
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    a| NASA technical note ; v| NASA TN D-8136
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    a| Prepared at NASA Flight Research Center.
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    a| Includes bibliographical references (p. 13).
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    a| Mode of access: Internet.
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    a| Airplanes x| Control systems.
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    a| Stability of airplanes.
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    a| Eagle (Jet fighter plane) x| Models x| Testing.
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    a| Shafer, Mary F.
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