Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 /

Nugent, Jack.
Powers, Bruce G.
United States. National Aeronautics and Space Administration.

"September 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Spectrometric measurements of gas temperatures in arc-heated jets and tunnels /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."October 1963"--Cover.Includes bibliographical references (p. 21...

Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 /

Runyan, Harry L.
Jones, Nan H.
Langley Research Center.

Prepared at the Langley Research Center, Langley Research Center.Cover title."June 1960."--Cover.Inc...

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...

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Prospects for obtaining aerodynamic heating results from analysis of meteor flight data /

Allen, H. Julian (Harry Julian), 1910-
James, Nataline A.
Ames Research Center.

Prepared at Ames Research Center."July 1964"--Cover.Includes bibliographical references (p. 53-56).M...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Spectrographic temperature measurements in a carbon-arc-powered air jet /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane /

Jones, Ira P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 26, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Heat-transfer measurements at a Mach number of 2 in the turbulent boundary layer on a flat plate having a stepwise temperature distribution /

Conti, Raul J. (Raul Jorge)
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Some observations of base heating at Mach 3.0 on a simulated missile with JP-4 liquid-oxygen rocket /

Samanich, Nick E.
Barnett, Donald D.
Lovell, J. Calvin.
Lewis Research Center.

January 1960

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

Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 /

Nugent, Jack.
Powers, Bruce G.
United States. National Aeronautics and Space Administration.

"September 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Spectrometric measurements of gas temperatures in arc-heated jets and tunnels /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."October 1963"--Cover.Includes bibliographical references (p. 21...

Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

Aerodynamic heating tests of missile stabilizers in a free jet at Mach number 2 /

Vosteen, Louis F.
Langley Research Center.

January 1960

"Declassified February 8, 1963.""September 1960."Cover title.Includes bibliographical references (p....

Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 /

Runyan, Harry L.
Jones, Nan H.
Langley Research Center.

Prepared at the Langley Research Center, Langley Research Center.Cover title."June 1960."--Cover.Inc...

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...

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Prospects for obtaining aerodynamic heating results from analysis of meteor flight data /

Allen, H. Julian (Harry Julian), 1910-
James, Nataline A.
Ames Research Center.

Prepared at Ames Research Center."July 1964"--Cover.Includes bibliographical references (p. 53-56).M...

Aerodynamic pressures and heating rates on surfaces between split elevons at Mach 6.6 /

Hunt, L. Roane (Lewis Roane)
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"December 1988"--Cover.Includes bibliographical references (p. 13).Mode of access: Internet

Spectrographic temperature measurements in a carbon-arc-powered air jet /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."December 1959."Cover title.Includes bibliographical references ...

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane /

Jones, Ira P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 26, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Heat-transfer measurements at a Mach number of 2 in the turbulent boundary layer on a flat plate having a stepwise temperature distribution /

Conti, Raul J. (Raul Jorge)
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Measurements of flow properties in the vicinity of three wing-fuselage combinations at Mach numbers of 1.61 and 2.01 /

Carlson, Harry W.
Langley Research Center.

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Some observations of base heating at Mach 3.0 on a simulated missile with JP-4 liquid-oxygen rocket /

Samanich, Nick E.
Barnett, Donald D.
Lovell, J. Calvin.
Lewis Research Center.

January 1960

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

Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 /

Nugent, Jack.
Powers, Bruce G.
United States. National Aeronautics and Space Administration.

"September 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Spectrometric measurements of gas temperatures in arc-heated jets and tunnels /

Greenshields, David H.
Langley Research Center.

Prepared at Langley Research Center."October 1963"--Cover.Includes bibliographical references (p. 21...

Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 /

Miller, Charles G. (Charles George), 1940-
Langley Research Center.

January 1984

Prepared at Langley Research Center."November 1984"--Cover.Includes bibliographical references (p. 1...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Abstract

Extracted data

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Abstract

Extracted data

Related items

Related items