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Three-Dimensional Supersonic Flutter Model Test Near Mach Number 1.5. Part III. Experimental and Theoretical Data for Wings with Control Surfaces.


AD118052

Publication Date 1958
Personal Author ASHER, G. W.; WEATHERILL, W. H.
Page Count 10
Abstract No abstract available.
Keywords
  • Wings
  • Flutter
  • Supersonic flow
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 46B - Fluid Mechanics
Corporate Authors Massachusetts Inst. of Tech., Cambridge. Aeroelastic and Structures Research Lab.
Document Type Technical Report
NTIS Issue Number 198104
Contract Number
  • AF33 038 22955
Three-Dimensional Supersonic Flutter Model Test Near Mach Number 1.5. Part III. Experimental and Theoretical Data for Wings with Control Surfaces.
Three-Dimensional Supersonic Flutter Model Test Near Mach Number 1.5. Part III. Experimental and Theoretical Data for Wings with Control Surfaces.
AD118052

  • Wings
  • Flutter
  • Supersonic flow
  • Non Paid Delimited ADS
  • 46B - Fluid Mechanics
  • AF33 038 22955
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