Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 /

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

An evaluation of two cooling-air ejectors in flight at transonic speeds /

Rolls, L. Stewart
Havill, C. Dewey, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "March 15, 1954."Includes bibliographical references.Mode of access: Internet

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of the NACA 4-(0)(03)-45 two-blade propeller at forward Mach numbers to 0.925 /

Carmel, Melvin M.
Milillo, Joseph R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"March 14, 1950."Includes bibliographical references (p. 0).Mode of access: Internet

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925 /

Delano, James B.
Harrison, Daniel E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1949

Investigations of the NACA-4-(4)(06)-04 two-blade propeller (design thickness, 0.06 at 0.7-radius st...

Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /

Canning, Thomas N.
Ames Research Center.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19, 1954."Includes bibliographical references (p. 12).Mode of access: Internet

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow /

Heath, Atwood R.
O'Neal, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 2, 1954."Includes bibliographical references (p. 14).Mode of access: Internet

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

Schulze, Wallace M.
Westphal, Willard R.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

The effect of high solidity on propeller characteristics at high forward speeds from wind-tunnel tests of the NACA 4-(3)(06.3)-06 and NACA 4-(3)(06.4)-09 two-blade propellers /

Delano, James B.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
Langley Aeronautical Laboratory.

January 1947

"February 27, 1947.""Langley Memorial Aeronautical Laboratory, Langley Field, Va."Cover title.Includ...

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

An evaluation of two cooling-air ejectors in flight at transonic speeds /

Rolls, L. Stewart
Havill, C. Dewey, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "March 15, 1954."Includes bibliographical references.Mode of access: Internet

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of the NACA 4-(0)(03)-45 two-blade propeller at forward Mach numbers to 0.925 /

Carmel, Melvin M.
Milillo, Joseph R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"March 14, 1950."Includes bibliographical references (p. 0).Mode of access: Internet

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96 /

Evans, Albert J.
Liner, George.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 30, 1953."Includes bibliographical references (p. 14).Mode of access: Internet

Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925 /

Delano, James B.
Harrison, Daniel E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1949

Investigations of the NACA-4-(4)(06)-04 two-blade propeller (design thickness, 0.06 at 0.7-radius st...

Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /

Canning, Thomas N.
Ames Research Center.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19, 1954."Includes bibliographical references (p. 12).Mode of access: Internet

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow /

Heath, Atwood R.
O'Neal, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 2, 1954."Includes bibliographical references (p. 14).Mode of access: Internet

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.Mode of access: Internet

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

Schulze, Wallace M.
Westphal, Willard R.
Erwin, John R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

The effect of high solidity on propeller characteristics at high forward speeds from wind-tunnel tests of the NACA 4-(3)(06.3)-06 and NACA 4-(3)(06.4)-09 two-blade propellers /

Delano, James B.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
Langley Aeronautical Laboratory.

January 1947

"February 27, 1947.""Langley Memorial Aeronautical Laboratory, Langley Field, Va."Cover title.Includ...

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

An evaluation of two cooling-air ejectors in flight at transonic speeds /

Rolls, L. Stewart
Havill, C. Dewey, joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "March 15, 1954."Includes bibliographical references.Mode of access: Internet

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 /

Abstract

Extracted data

Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 /

Abstract

Extracted data

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