Search Results

1

A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14 /

by Carlson, Harry W., Mack, Robert J.
[Washington] : Springfield Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document Book

2

Application of sonic-boom minimization concepts in supersonic transport design /

by Carlson, Harry W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

3

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /

by Carlson, Harry W.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

4

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

by Mack, Robert J.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1988

Government Document Book

5

Estimation of leading-edge thrust for supersonic wings of arbitrary planform /

by Carlson, Harry W., Mack, Robert J.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service., 1978

Government Document Book

6

An improved method for calculating supersonic pressure fields about bodies of revolution /

by Mack, Robert J.
Washington, D.C. : National Aeronautics and Space Administration, 1971

Government Document Book

7

Supersonic wings with significant leading-edge thrust at cruise /

by Robins, A. Warner
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book

8

Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 /

by Mack, Robert J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

9

Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 /

by Morris, Odell A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1968

Government Document Book

10

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

by Mack, Robert J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

11

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

by Mack, Robert J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book

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