A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).Mode of access: Internet

Bypass-duct design for use with supersonic inlets /

Wood, Charles C.
Henry, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"March 16, 1956".Includes bibliographical references (p. 6).Mode of access: Internet

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

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

An experimental study of five annular air inlet configurations at subsonic and transonic speeds /

Bryan, Carroll R.
Fleming, Frank F.
Milillo, Jospeh R.
Pendley, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 19, 1953."Includes bibliographical references (p. 22-23).Mode of access: Internet

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).Mode of access: Internet

The use of perforated inlets for efficient supersonic diffusion /

Evvard, John C.
Blakey, John W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

On front cover: "April 13, 1951."Cover title.Includes bibliographical references: p. 16-17.Mode of a...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

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

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).Mode of access: Internet

Bypass-duct design for use with supersonic inlets /

Wood, Charles C.
Henry, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"March 16, 1956".Includes bibliographical references (p. 6).Mode of access: Internet

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

Carlson, Harry W.
Mack, Robert J.
Barger, Raymond L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 42-44.Mode of access: Internet

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

An experimental study of five annular air inlet configurations at subsonic and transonic speeds /

Bryan, Carroll R.
Fleming, Frank F.
Milillo, Jospeh R.
Pendley, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 19, 1953."Includes bibliographical references (p. 22-23).Mode of access: Internet

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).Mode of access: Internet

The use of perforated inlets for efficient supersonic diffusion /

Evvard, John C.
Blakey, John W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

On front cover: "April 13, 1951."Cover title.Includes bibliographical references: p. 16-17.Mode of a...

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /

Trefny, Charles J.
Wasserbauer, Joseph W.
Lewis Research Center.

January 1986

Prepared at Lewis Research Center."February 1986"--Cover.Includes bibliographical references (p. 10)...

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

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

A methodology for designing aircraft to low sonic boom constraints /

Mack, Robert J.
Needleman, Kathy E.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Includes bibliographical references (p. 6).Mode of access: Inter...

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.Mode of access: Internet

Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body /

Sleeman, William C.
Robins, A. Warner.
Langley Research Center.

Cover title.Includes bibliographical references (p. 18).Mode of access: Internet

Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /

Reller, John O. Jr.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 16, 1957."Includes bibliographical references: p. 6-7.Mode of access: Intern...

Inlet sensitivity study for a supersonic transport /

Koenig, Robert W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

"March 1967."Includes bibliographical references (p. 52).Mode of access: Internet

A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

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A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds /

Abstract

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