Investigation of drag reduction by boundary-layer suction on a flat plate and a 36-deg swept wing at supersonic speeds /

Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing /

Bray, Richard S.
Innis, Robert C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a le...

Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock /

Shoemaker, Charles J.
Henry, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Propulsion system elements; Propulsion systems, air...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Investigation of drag reduction by boundary-layer suction on a body of revolution at Mach numbers 2.5, 3, and 3.5 /

Pate, S. R., author.
ARO, Inc. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Arnold Engineering Development Center. issuing body.

"Research supported by the United States Air Force, and performed by the Von Karman Gas Dynamics Fac...

Investigation of boundary-layer transition on swept wings at mach numbers 2.5 to 5 /

Pate, S. R., author.
Brillhart, R. E., author.
Sverdrup/ARO, Inc. AEDC Division. sponsor.
Arnold Engineering Development Center. issuing body

"Research conducted by the von Kármán Gas Dynamics Facility, ARO, In.""ARO Project No. VD0318.""AFSC...

Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4 /

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

Tests were conducted in the 40-in. supersonic Tunnel A of the von Karman Gas Dynamics Facility to de...

The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 /

Pate, S. R., author.
ARO, Inc. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62405334, Project No. 1366.""May 1965."Includes bibliographical references (page 5)...

Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 /

Strike, W. T., author.
Pate, S., author.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.
Arnold Engineering Development Center. issuing body.

A second investigation was conducted in the 12in., intermittent, supersonic wind tunnel of the von K...

An experimental investigation of boundary-layer control for drag reduction of a swept-wing section at low speed and high reynolds numbers. /

Gault, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode...

Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities /

Lamb, Milton.
Stallings, Robert L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Preliminary experimental results of the reduction of viscous effects in a low-density supersonic nozle by wall cryopumping /

MacDermott, W. N., author.
Arnold Engineering Development Center. issuing body.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.

"AFSC Program Area 750A, Project 8950, Task 89602.""ARO Project No. 506104.""October 1961."Includes ...

Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90 /

Saltzman, Edwin J.
Hintz, John.
Flight Research Center (U.S.)

January 1967

"NASA TM X-1376.""Flight Research Center, Edwards, Calif.""May 1967"--Cover.Includes bibliographical...

Aerodynamic investigation of submunition stabiliation, retardation and dispersion concepts /

Brunk, James E., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Research conducted by the Alpha Research, Inc., Santa Barbara, California.""July 1974."Includes bib...

Analytical and design techniques for drag reduction studies on wavy surfaces /

Balasubramanian, R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Prepared for Langley Research Center under contract NAS1-15278."Includes bibliographical references...

Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow /

Boylan, David E., author.
Sims, William H., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Report prepared by ARO, Inc., a subsidiary of Sverdrup and Parcel, Inc."April 1964."Includes bibliog...

Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing /

Bray, Richard S.
Innis, Robert C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a le...

Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock /

Shoemaker, Charles J.
Henry, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Propulsion system elements; Propulsion systems, air...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Investigation of drag reduction by boundary-layer suction on a body of revolution at Mach numbers 2.5, 3, and 3.5 /

Pate, S. R., author.
ARO, Inc. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Arnold Engineering Development Center. issuing body.

"Research supported by the United States Air Force, and performed by the Von Karman Gas Dynamics Fac...

Investigation of boundary-layer transition on swept wings at mach numbers 2.5 to 5 /

Pate, S. R., author.
Brillhart, R. E., author.
Sverdrup/ARO, Inc. AEDC Division. sponsor.
Arnold Engineering Development Center. issuing body

"Research conducted by the von Kármán Gas Dynamics Facility, ARO, In.""ARO Project No. VD0318.""AFSC...

Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4 /

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

Tests were conducted in the 40-in. supersonic Tunnel A of the von Karman Gas Dynamics Facility to de...

The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 /

Pate, S. R., author.
ARO, Inc. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Arnold Engineering Development Center. issuing body.

"Program Element 62405334, Project No. 1366.""May 1965."Includes bibliographical references (page 5)...

Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 /

Strike, W. T., author.
Pate, S., author.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.
Arnold Engineering Development Center. issuing body.

A second investigation was conducted in the 12in., intermittent, supersonic wind tunnel of the von K...

An experimental investigation of boundary-layer control for drag reduction of a swept-wing section at low speed and high reynolds numbers. /

Gault, Donald E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mode...

Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities /

Lamb, Milton.
Stallings, Robert L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Preliminary experimental results of the reduction of viscous effects in a low-density supersonic nozle by wall cryopumping /

MacDermott, W. N., author.
Arnold Engineering Development Center. issuing body.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.

"AFSC Program Area 750A, Project 8950, Task 89602.""ARO Project No. 506104.""October 1961."Includes ...

Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90 /

Saltzman, Edwin J.
Hintz, John.
Flight Research Center (U.S.)

January 1967

"NASA TM X-1376.""Flight Research Center, Edwards, Calif.""May 1967"--Cover.Includes bibliographical...

Aerodynamic investigation of submunition stabiliation, retardation and dispersion concepts /

Brunk, James E., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Research conducted by the Alpha Research, Inc., Santa Barbara, California.""July 1974."Includes bib...

Analytical and design techniques for drag reduction studies on wavy surfaces /

Balasubramanian, R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"Prepared for Langley Research Center under contract NAS1-15278."Includes bibliographical references...

Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow /

Boylan, David E., author.
Sims, William H., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Report prepared by ARO, Inc., a subsidiary of Sverdrup and Parcel, Inc."April 1964."Includes bibliog...

Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing /

Bray, Richard S.
Innis, Robert C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

Tests have been made to determine the flight characteristics of an F-86F airplane equipped with a le...

Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock /

Shoemaker, Charles J.
Henry, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Propulsion system elements; Propulsion systems, air...

Study to determine aerodynamic characteristics on hypersonic re-entry configurations.

Malvestuto, Frank S., Jr., author.
Huggins, Vivan E., author.
Larrivee, Jules A. (Jules Alphonse), 1909-. author.
Mortzschky, Herbert A., author.
Marcy, William L., author.
Sullivan, Phillip J., author.
Lockheed Aircraft Corporation. sponsor.
United States. Air Force. Systems Command. Aeronautical Systems Division. issuing sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.

"Project No. 1366, Task No. 136608.""August 1962."Includes bibliographical references (pages 247-265...

Investigation of drag reduction by boundary-layer suction on a flat plate and a 36-deg swept wing at supersonic speeds /

Abstract

Extracted data

Investigation of drag reduction by boundary-layer suction on a flat plate and a 36-deg swept wing at supersonic speeds /

Abstract

Extracted data

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