Item Details

Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting-Mass Flutter Suppressor

by E. Carson Yates, Jr.
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1960]
Language
English
Series
NASA Technical Note
Description
45 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • Cover title.
  • "November 1960."
  • Stresses and loads.
  • Includes bibliographical references.
Series Statement
NASA technical note ; NASA TN D-542
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor / c| by E. Carson Yates, Jr.
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