Dynamics of high-drag probe shapes at transonic speeds /

Performance of a mass-flux probe in a Mach 3 stream /

Krause, Lloyd N.
Glawe, George E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Performance of mass flux probe in Mach 3 stream.Prepared at Lewis Research Center."November 1969."Co...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Project No. 3066, Task No. 306611.""Final Report, Supplement I.""November 1968."Includes bibliograp...

An aerodynamic and hydrodynamic investigation of two multi-jet water-based aircraft having low transonic drag rise /

Olson, Roland E.
Bielat, Ralph P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 15, 1955; Declassified May 29, 1959."Includes bibliographical references (p. 16-17).Mode o...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe /

Malcolm, Gerald N.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."April 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

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

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Drag measurements at transonic speeds of two bodies of fineness ratio 9 with different locations of maximum body diameter /

Thompson, Jim Rogers.
Kurbjun, Max C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 22, 1948."Includes bibliographical references (p. 7).Mode of access: Internet

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3 /

Wallskog, Harvey A.
Hart, Roger G.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 11, 1953."Includes bibliographical references (p. 12-13).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

Studies of optimum body shapes at hypersonic speeds /

Stivers, Louis S., Jr.
Spender, Bernard, Jr.
Langley Research Center.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center and Langley Research Center."N67-40121."Includes bibliographical re...

Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds /

Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

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)....

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Final Report.""Project No. 3066, Task No. 306611.""November 1968."Includes bibliographical referenc...

Performance of a mass-flux probe in a Mach 3 stream /

Krause, Lloyd N.
Glawe, George E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Performance of mass flux probe in Mach 3 stream.Prepared at Lewis Research Center."November 1969."Co...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Project No. 3066, Task No. 306611.""Final Report, Supplement I.""November 1968."Includes bibliograp...

An aerodynamic and hydrodynamic investigation of two multi-jet water-based aircraft having low transonic drag rise /

Olson, Roland E.
Bielat, Ralph P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 15, 1955; Declassified May 29, 1959."Includes bibliographical references (p. 16-17).Mode o...

Drag of a supercritical body of revolution in free flight at transonic speeds and comparison with wind-tunnel data /

Usry, J. W.
Wallace, John W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."December 1971."Includes bibliographical references (p. 13).Mode...

Stability and drag characteristics at Mach numbers of 10 and 26 of a proposed slender atmospheric probe /

Malcolm, Gerald N.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."April 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Longitudinal aerodynamic characteristics of several high-drag bodies at Mach numbers from 1.50 to 4.63 /

Campbell, James F.
United States. National Aeronautics and Space Administration.

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

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Drag measurements at transonic speeds of two bodies of fineness ratio 9 with different locations of maximum body diameter /

Thompson, Jim Rogers.
Kurbjun, Max C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 22, 1948."Includes bibliographical references (p. 7).Mode of access: Internet

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3 /

Wallskog, Harvey A.
Hart, Roger G.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 11, 1953."Includes bibliographical references (p. 12-13).Mode of access: Internet

Experimental aerodynamic performance characteristics of a rotor entry vehicle configuration : II. Transonic /

Levin, Alan D.
Smith, Ronald C. (Ronald Carlton)
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1971

Prepared at Ames Research Center.N71-16534.February 1971.Includes bibliographical references (p. 9)....

Studies of optimum body shapes at hypersonic speeds /

Stivers, Louis S., Jr.
Spender, Bernard, Jr.
Langley Research Center.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center and Langley Research Center."N67-40121."Includes bibliographical re...

Drag measurements of blunt stores tangentially mounted on a flat plate at supersonic speeds /

Wilcox, Floyd J. (Floyd Jay)
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

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)....

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Final Report.""Project No. 3066, Task No. 306611.""November 1968."Includes bibliographical referenc...

Performance of a mass-flux probe in a Mach 3 stream /

Krause, Lloyd N.
Glawe, George E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

Performance of mass flux probe in Mach 3 stream.Prepared at Lewis Research Center."November 1969."Co...

Experimental evaluation of inlet drag characteristics in the transonic mach number regime /

McVey, F. D., author.
Phillips, E. J., author.
Rejeske, J. V., author.
McDonnell Douglas Corporation. sponsor.
United States. Air Force. Systems Command. sponsor.
Air Force Aero Propulsion Laboratory (U.S.). issuing body.

"Project No. 3066, Task No. 306611.""Final Report, Supplement I.""November 1968."Includes bibliograp...

An aerodynamic and hydrodynamic investigation of two multi-jet water-based aircraft having low transonic drag rise /

Olson, Roland E.
Bielat, Ralph P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 15, 1955; Declassified May 29, 1959."Includes bibliographical references (p. 16-17).Mode o...

Dynamics of high-drag probe shapes at transonic speeds /

Abstract

Extracted data

Dynamics of high-drag probe shapes at transonic speeds /

Abstract

Extracted data

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