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Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1. Model Design and Testing Techniques.


AD103035

Publication Date 1955
Personal Author MCCARTHY, J. F.; ASHER, G. W.
Page Count 10
Abstract No abstract available.
Keywords
  • Wind tunnel models
  • Wings
  • Flutter
  • Model tests
  • Supersonic flow
  • Test methods
Source Agency
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
Corporate Authors Massachusetts Inst. of Tech., Cambridge. Aeroelastic and Structures Research Lab.
Document Type Technical Report
NTIS Issue Number 198101
Contract Number
  • AF33 038 22955
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1. Model Design and Testing Techniques.
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1. Model Design and Testing Techniques.
AD103035

  • Wind tunnel models
  • Wings
  • Flutter
  • Model tests
  • Supersonic flow
  • Test methods
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
  • AF33 038 22955
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