Procedure used for X-15 heat transfer and pressure distribution tests at hypersonic speeds /

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 9...

Pressure distribution on a body a revolution in supersonic flight, by Robert R. Reynolds.

Reynolds, Robert Ramon.

January 1952

"This report appears as an appendix to the National Applied Mathematics Laboratories Quarterly repor...

An Analytical study of the use of air-equivalent hot gaseous mixtures for aerodynamic test purposes /

Tempelmeyer, Kenneth E., author.
ARO, Inc. sponsor.
Arnold Engineering Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"ARO Project No. 632032.""ASTIA Document No. AD-210866.""March 1959."Includes bibliographical refere...

Operational and performance characteristics of the X-15 spherical, hypersonic flow-direction sensor /

Wolowicz, Chester H.
Gossett, Terrence D.
Flight Research Center (U.S.)

Prepared at Flight Research Center."November 1965"--Cover.Includes bibliographical references (p. 18...

Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls.

Kaufman, Louis G., II., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Grumman Aircraft Engineering Corporation. Research Department. sponsor.

Includes bibliograpical references (pages 7-8 ).Air Force Contract No.Mode of access: Internet

Hypersonic research summary.

Fabian, Gardner J.

January 1960

"Contract AF 18(603)-141. Mechanics Division, Air Force Office of Scientific Research, Air Research ...

Sound and pressure measurements in cavities on a body of revolution at supersonic speeds /

Donaldson, J. C., author.
Bell, D. R., author.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.
Arnold Engineering Development Center. issuing body.

"Research supported by the United States Air Force, and performed by the VKF, ARO, Inc.""ARO Project...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

Flow visualization techniques for use in hypersonic wind tunnels /

Rhudy, R. W., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"October 1964."Includes bibliograqphic references (page 8).Report prepared by ARO, Inc., under Air F...

Pressure distribution of a 0.0667-scale model of the X-15 airplane for an angle-of-attack range of 0° to 28° at mach numbers of 2.30, 288, and 4.65 /

Hodge, B. Leon.
Burbank, Paige B.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

A Study of laminar heat transfer to spherically blunted cones and hemisphere-cylinders at hypersonic conditions /

Griffith, B. J., author.
Lewis, Clark H. (Clark Houston), 1929-. author.
Sverdrup/ARO, Inc. AEDC Division. sponsor.
Arnold Engineering Development Center. issuing body

"Research conducted at the von Kármán Gas Dynamics Facility, ARO, Inc.""ARO Project No. VT2149.""AFS...

Inviscid hypersonic flow over a blunt body with high rates of mass and heat transfer /

Martin, E. Dale (Elmer Dale)
Ames Research Center.

Prepared at Ames Research Center."March 1968"--Cover.Includes bibliographical references (p. 30-31)....

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /

Holloway, Paul F.
Creekmore, Helen S.
Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."November 1965"--Cover.Includes bibliographical references (p. 3...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 9...

Pressure distribution on a body a revolution in supersonic flight, by Robert R. Reynolds.

Reynolds, Robert Ramon.

January 1952

"This report appears as an appendix to the National Applied Mathematics Laboratories Quarterly repor...

An Analytical study of the use of air-equivalent hot gaseous mixtures for aerodynamic test purposes /

Tempelmeyer, Kenneth E., author.
ARO, Inc. sponsor.
Arnold Engineering Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"ARO Project No. 632032.""ASTIA Document No. AD-210866.""March 1959."Includes bibliographical refere...

Operational and performance characteristics of the X-15 spherical, hypersonic flow-direction sensor /

Wolowicz, Chester H.
Gossett, Terrence D.
Flight Research Center (U.S.)

Prepared at Flight Research Center."November 1965"--Cover.Includes bibliographical references (p. 18...

Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls.

Kaufman, Louis G., II., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Grumman Aircraft Engineering Corporation. Research Department. sponsor.

Includes bibliograpical references (pages 7-8 ).Air Force Contract No.Mode of access: Internet

Hypersonic research summary.

Fabian, Gardner J.

January 1960

"Contract AF 18(603)-141. Mechanics Division, Air Force Office of Scientific Research, Air Research ...

Sound and pressure measurements in cavities on a body of revolution at supersonic speeds /

Donaldson, J. C., author.
Bell, D. R., author.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.
Arnold Engineering Development Center. issuing body.

"Research supported by the United States Air Force, and performed by the VKF, ARO, Inc.""ARO Project...

Preliminary base pressures obtained from the X-15 airplane at mach numbers from 1.1 to 3.2 /

Saltzman, Edwin J.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles; Vehicle ...

Flow visualization techniques for use in hypersonic wind tunnels /

Rhudy, R. W., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

"October 1964."Includes bibliograqphic references (page 8).Report prepared by ARO, Inc., under Air F...

Pressure distribution of a 0.0667-scale model of the X-15 airplane for an angle-of-attack range of 0° to 28° at mach numbers of 2.30, 288, and 4.65 /

Hodge, B. Leon.
Burbank, Paige B.
United States. National Aeronautics and Space Administration.

"May 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

A Study of laminar heat transfer to spherically blunted cones and hemisphere-cylinders at hypersonic conditions /

Griffith, B. J., author.
Lewis, Clark H. (Clark Houston), 1929-. author.
Sverdrup/ARO, Inc. AEDC Division. sponsor.
Arnold Engineering Development Center. issuing body

"Research conducted at the von Kármán Gas Dynamics Facility, ARO, Inc.""ARO Project No. VT2149.""AFS...

Inviscid hypersonic flow over a blunt body with high rates of mass and heat transfer /

Martin, E. Dale (Elmer Dale)
Ames Research Center.

Prepared at Ames Research Center."March 1968"--Cover.Includes bibliographical references (p. 30-31)....

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 /

Holloway, Paul F.
Creekmore, Helen S.
Sterrett, James R.
Langley Research Center.

Prepared at Langley Research Center."November 1965"--Cover.Includes bibliographical references (p. 3...

Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 /

Anderson, K. G., author.
Durben, J. M., author.
Merrell, H. B., author.
Wright Air Development Center. issuing body.
United States. Air Force. Air Research and Development Command. sponsor.

"December 1951."Includes bibliographical references (pages 45-47).Aero Medical Laboratory Contract N...

Basic pressure measurements on a 0.0667-scale model of the North American X-15 research airplane at transonic speeds /

Osborne, Robert S.
Stafford, Virginia C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""October 1960."Cover title.Includes bibliographical ref...

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 /

Glass, Christopher E. (Christopher Earl), 1955-
Hunt, L. Roane (Lewis Roane)
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 9...

Pressure distribution on a body a revolution in supersonic flight, by Robert R. Reynolds.

Reynolds, Robert Ramon.

January 1952

"This report appears as an appendix to the National Applied Mathematics Laboratories Quarterly repor...

Procedure used for X-15 heat transfer and pressure distribution tests at hypersonic speeds /

Abstract

Extracted data

Procedure used for X-15 heat transfer and pressure distribution tests at hypersonic speeds /

Abstract

Extracted data

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