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

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

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...

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

Osborne, Robert S.
Kelly, Thomas C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"April 9, 1953."Includes bibliographical references (p. 7-9).Mode of access: Internet

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45©� sweptback wing of aspect ratio 4 and a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96 /

Jacobsen, Carl R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 21, 1953."Includes bibliographical references (p. 8-9).Mode of access: Internet

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

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

Loads on wings due to spoilers at subsonic and transonic speeds /

Hammond, Alexander D.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 27, 1955; Declassified September 1, 1959."Includes bibliographical references (p. 7).Mode of a...

Transonic flutter investigation of two 50©� semispan modified-delta wings with tip ailerons /

Platt, Robert J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"February 17, 1958."Includes bibliographical references (p. 6).Mode of access: Internet

Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds /

Matranga, Gene J.
Armistead, Katharine H.
Flight Research Center (U.S.)
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"March 6, 1958."Includes bibliographical references (p. 10).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

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

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

Transonic longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a rocket-propelled airplane model having no horizontal tail /

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

January 1955

"January 20, 1955."Includes bibliographical references (p. 12-13).Mode of access: Internet

A transonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution /

Holdaway, George H.
Hatfield, Elaine W., joint author.
Wallace, Minor R., Jr. joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "October 28, 1957."Includes bibliographical references: p. 9.Mode of access: Interne...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

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...

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

Osborne, Robert S.
Kelly, Thomas C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"April 9, 1953."Includes bibliographical references (p. 7-9).Mode of access: Internet

Flight measurement of the stability characteristics of the Douglas D-558-1 airplane (Buaero no. 37971) in sideslips /

Williams, Walter C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"April 18, 1949."Includes bibliographical references (p. 5).Mode of access: Internet

Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45©� sweptback wing of aspect ratio 4 and a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96 /

Jacobsen, Carl R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 21, 1953."Includes bibliographical references (p. 8-9).Mode of access: Internet

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

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

Loads on wings due to spoilers at subsonic and transonic speeds /

Hammond, Alexander D.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 27, 1955; Declassified September 1, 1959."Includes bibliographical references (p. 7).Mode of a...

Platt, Robert J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"February 17, 1958."Includes bibliographical references (p. 6).Mode of access: Internet

Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds /

Matranga, Gene J.
Armistead, Katharine H.
Flight Research Center (U.S.)
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"March 6, 1958."Includes bibliographical references (p. 10).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

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

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

Transonic longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a rocket-propelled airplane model having no horizontal tail /

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

January 1955

"January 20, 1955."Includes bibliographical references (p. 12-13).Mode of access: Internet

A transonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution /

Holdaway, George H.
Hatfield, Elaine W., joint author.
Wallace, Minor R., Jr. joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "October 28, 1957."Includes bibliographical references: p. 9.Mode of access: Interne...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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