A note on the drag due to lift of delta wings at Mach numbers up to 2.0 /

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

Riebe, John M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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

Large-scale flight measurements of zero-lift drag and low-lift drag of 10 wing-body configurations at Mach numbers from 0.8 to 1.6 /

Morrow, John D.
Nelson, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 15, 1953."Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

Dunning, Robert W.
Smith, Fred M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1959

"June 11, 1953; Declassified August 26, 1959."Includes bibliographical references (p. 6).Mode of acc...

Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds /

Sandahl, Carl A.
Stoney, William E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 18, 1954."Includes bibliographical references (p. 11).Mode of access: Internet

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).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

Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves /

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

January 1949

"February 23, 1949."Includes bibliographical references (p. 12).Mode of access: Internet

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Effect of wing-mounted external stores on the lift and drag of the Douglas D-558-II research airplane at transonic speeds /

Nugent, Jack.
Flight Research Center (U.S.)
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"July 17, 1957."Includes bibliographical references (p. 10).Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

Riebe, John M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

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

Large-scale flight measurements of zero-lift drag and low-lift drag of 10 wing-body configurations at Mach numbers from 0.8 to 1.6 /

Morrow, John D.
Nelson, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 15, 1953."Includes bibliographical references (p. 12-13).Mode of access: Internet

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

Dunning, Robert W.
Smith, Fred M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1959

"June 11, 1953; Declassified August 26, 1959."Includes bibliographical references (p. 6).Mode of acc...

Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds /

Sandahl, Carl A.
Stoney, William E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"February 18, 1954."Includes bibliographical references (p. 11).Mode of access: Internet

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).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

Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves /

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

January 1949

"February 23, 1949."Includes bibliographical references (p. 12).Mode of access: Internet

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Effect of wing-mounted external stores on the lift and drag of the Douglas D-558-II research airplane at transonic speeds /

Nugent, Jack.
Flight Research Center (U.S.)
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"July 17, 1957."Includes bibliographical references (p. 10).Mode of access: Internet

Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing /

Keener, Earl R.
Flight Research Center (U.S.)

January 1959

"October 1959."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

Riebe, John M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

A note on the drag due to lift of delta wings at Mach numbers up to 2.0 /

Abstract

Extracted data

A note on the drag due to lift of delta wings at Mach numbers up to 2.0 /

Abstract

Extracted data

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