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Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental and Theoretical Data for Bare Wings and Wings with Tip Tanks.


AD110593

Publication Date 1955
Personal Author McCarthy, J. F.; Zartarian, G.
Page Count 250
Abstract No abstract available.
Keywords
  • Wings
  • Flutter
  • Model tests
  • Supersonic flow
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 51A - Aerodynamics
Corporate Authors Massachusetts Inst Of Tech Cambridge Aeroelastic And Structures Research Lab
Document Type Technical Report
NTIS Issue Number 197620
Contract Number
  • AF33 038 22955
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental and Theoretical Data for Bare Wings and Wings with Tip Tanks.
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental and Theoretical Data for Bare Wings and Wings with Tip Tanks.
AD110593

  • Wings
  • Flutter
  • Model tests
  • Supersonic flow
  • Non Paid Delimited ADS
  • 51A - Aerodynamics
  • AF33 038 22955
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