Calculation of supersonic flows at large distances from slender lifting bodies /

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN IV routines /

Johnson, Robert C. (Robert Clinton), 1924-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 86-87).Mode of...

Calculation of compressible potential flow past slender bodies of revolution by an integral method /

Klein, Milton M.
Perl, W.
United States. National Advisory Committee for Aeronautics.

January 1950

An integral method, previously used to obtain compressible flow past two-dimensional shapes, is appl...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

Calculation of supersonic flows at large distances from slender lifting bodies

Schorling, M.

August 1971

Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodie

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

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

Mack, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Development of near-field method for determining supersonic flow properties about bodies of revoluti...

Supersonic aerodynamic characteristics and shock standoff distances for large-angle cones with and without cylindrical afterbodies /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and w...

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

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones /

Briggs, Benjamin R.
Ames Research Center.

January 1959

"NASA TN D-24.""Ames Research Center, Moffett Field, Calif.""August 1959."Title from cover.Includes ...

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique /

Marconi, Frank.
Yaeger, Larry, joint author.
Salas, Manuel, joint author.
United States. National Aeronautics and Space Administration.
Grumman Aerospace Corporation.

January 1976

Cover title.Includes bibliographical references (p. 87-88).Mode of access: Internet

Computation of equilibrium hypersonic flow about blunt axisymmetric bodies with sharp concers : (Final Report) /

Curtis, J. T., author.
Strom, C. R., author.
Sandia Corporation
U.S. Atomic Energy Commission.

"Purchase Orders 4804, Suborder 10 and 5003, Suborder 9.""August 1967."Includes bibliographical refe...

Kinetic study of the hypersonic flow past the leading edge of a flat plate.

El Assar, Rateb Jaber, 1937-

January 1968

Vita.Includes bibliographical references (leaves 48-52).Mode of access: Internet

Supersonic flow past a family of blunt axisymmetric bodies /

Van Dyke, Milton.
Gordon, Helen D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1959

Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached...

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN IV routines /

Johnson, Robert C. (Robert Clinton), 1924-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 86-87).Mode of...

Calculation of compressible potential flow past slender bodies of revolution by an integral method /

Klein, Milton M.
Perl, W.
United States. National Advisory Committee for Aeronautics.

January 1950

An integral method, previously used to obtain compressible flow past two-dimensional shapes, is appl...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

Calculation of supersonic flows at large distances from slender lifting bodies

Schorling, M.

August 1971

Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodie

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners : including a program description and listing /

South, Jerry C. (Jerry Curtis), 1935-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 36-37).Mode of access: Internet

Numerical solutions for supersonic flow of an ideal gas around blunt two-dimensional bodies /

Fuller, Franklyn B.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mec...

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

Mack, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Development of near-field method for determining supersonic flow properties about bodies of revoluti...

Supersonic aerodynamic characteristics and shock standoff distances for large-angle cones with and without cylindrical afterbodies /

Campbell, James F. (James Franklin), 1941-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and w...

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

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones /

Briggs, Benjamin R.
Ames Research Center.

January 1959

"NASA TN D-24.""Ames Research Center, Moffett Field, Calif.""August 1959."Title from cover.Includes ...

Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique /

Marconi, Frank.
Yaeger, Larry, joint author.
Salas, Manuel, joint author.
United States. National Aeronautics and Space Administration.
Grumman Aerospace Corporation.

January 1976

Cover title.Includes bibliographical references (p. 87-88).Mode of access: Internet

Computation of equilibrium hypersonic flow about blunt axisymmetric bodies with sharp concers : (Final Report) /

Curtis, J. T., author.
Strom, C. R., author.
Sandia Corporation
U.S. Atomic Energy Commission.

"Purchase Orders 4804, Suborder 10 and 5003, Suborder 9.""August 1967."Includes bibliographical refe...

Kinetic study of the hypersonic flow past the leading edge of a flat plate.

El Assar, Rateb Jaber, 1937-

January 1968

Vita.Includes bibliographical references (leaves 48-52).Mode of access: Internet

Supersonic flow past a family of blunt axisymmetric bodies /

Van Dyke, Milton.
Gordon, Helen D.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1959

Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached...

A method for determining surface pressures on blunt bodies of revolution at small angles of attack in supersonic flow /

Jackson, Charlie M.
Smith, Rudeen S.
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration.

Cover title."November 1968."Includes bibliographical references.Mode of access: Internet

Calculation of supersonic stream parameters of a real gas from measurable quantities using FORTRAN IV routines /

Johnson, Robert C. (Robert Clinton), 1924-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 86-87).Mode of...

Calculation of compressible potential flow past slender bodies of revolution by an integral method /

Klein, Milton M.
Perl, W.
United States. National Advisory Committee for Aeronautics.

January 1950

An integral method, previously used to obtain compressible flow past two-dimensional shapes, is appl...

Second-order small-disturbance solutions for hypersonic flow over power-law bodies /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 57-58).Mode ...

Calculation of supersonic flows at large distances from slender lifting bodies /

Abstract

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Calculation of supersonic flows at large distances from slender lifting bodies /

Abstract

Extracted data

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