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Development of Subsonic Base Pressure Prediction Methods, Volume II.


AD475671

Publication Date 1965
Personal Author Butsko, J. E.; Carter, W. V.; Herman, W.
Page Count 122
Abstract The results are presented of the wind tunnel test. The methods and scope of the experimental investigation are presented, as well as, the tabulated, plotted and photographic data obtained. (Author)
Keywords
  • Base pressure
  • Subsonic flow
  • Subsonic characteristics
  • Aerodynamic configurations
  • Wind tunnel models
  • Model tests
  • Performance(Engineering)
  • Flow visualization
  • Wake
  • Force(Mechanics)
  • Moments
  • Flow fields
  • Reynolds number
  • Blunt bodies
  • Pressure
  • Wings
  • Trailing edge
  • Wing body configurations
  • Leading edges
  • Delta wings
  • Sweptback wings
  • Afterbodies
  • Fins
  • Flared afterbodies
  • Boundary layer transition
  • Experimental data
  • Test methods
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 46B - Fluid Mechanics
Corporate Authors General Dynamics/Convair, San Diego, CA.
Supplemental Notes See also Vol-1, AD-475 670.
Document Type Technical Report
Title Note Final rept.
NTIS Issue Number 198009
Contract Number
  • AF33(615)-1615
Development of Subsonic Base Pressure Prediction Methods, Volume II.
Development of Subsonic Base Pressure Prediction Methods, Volume II.
AD475671

  • Base pressure
  • Subsonic flow
  • Subsonic characteristics
  • Aerodynamic configurations
  • Wind tunnel models
  • Model tests
  • Performance(Engineering)
  • Flow visualization
  • Wake
  • Force(Mechanics)
  • Moments
  • Flow fields
  • Reynolds number
  • Blunt bodies
  • Pressure
  • Wings
  • Trailing edge
  • Wing body configurations
  • Leading edges
  • Delta wings
  • Sweptback wings
  • Afterbodies
  • Fins
  • Flared afterbodies
  • Boundary layer transition
  • Experimental data
  • Test methods
  • Non Paid Delimited ADS
  • 46B - Fluid Mechanics
  • AF33(615)-1615
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