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Dollyhigh, Samuel M.
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Fighter planes

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Current results range from 1974 to 1979

1.
Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations
Author
Dollyhigh, Samuel M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
2.
Effects of stores on longitudinal aerodynamic characteristics of a fighter at supersonic speeds
Author
Dollyhigh, Samuel M.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
3.
Subsonic and supersonic longitudinal stability and control characteristics of an aft-tail fighter configuration with cambered and uncambered wings and cambered fuselage
Author
Dollyhigh, Samuel M.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
4.
Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage
Author
Dollyhigh, Samuel M.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online