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

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).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

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

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).Mode of access: Internet

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

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

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Longitudinal stability and trim of two rocket-propelled airplane models having 45©� sweptback wings and tails with the horizontal tail mounted in two positions /

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

January 1953

"December 9, 1953."Includes bibliographical references (p. 8).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...

Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45©� sweptback wing-fuselage model /

Solomon, William.
Schmeer, James W.
United States. National Advisory Committee for Aeronautics.

"March 4, 1953."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule /

Palmer, William E.
Braslow, Albert L.
Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"July 20, 1956."Includes bibliographical references (p. 11).Mode of access: Internet

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).Mode of access: Internet

Effects of a sweptback hydrofoil on the force and longitudinal stability characteristics of a typical high-speed airplane /

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

January 1948

"December 2, 1948."Includes bibliographical references (p. 7).Mode of access: Internet

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

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

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).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

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

Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail /

Hieser, Gerald.
Reid, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 15, 1956."Includes bibliographical references (p. 17-18).Mode of access: Internet

Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing /

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

January 1952

"April 11, 1952."Includes bibliographical references (p. 15-16).Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings /

Luoma, Arvo A.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 14-15).Mode of access: Internet

Longitudinal stability and trim of two rocket-propelled airplane models having 45©� sweptback wings and tails with the horizontal tail mounted in two positions /

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

January 1953

"December 9, 1953."Includes bibliographical references (p. 8).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...

Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45©� sweptback wing-fuselage model /

Solomon, William.
Schmeer, James W.
United States. National Advisory Committee for Aeronautics.

"March 4, 1953."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Longitudinal aerodynamic characteristics at transonic speeds of a V/STOL airplane configuration with a fixed delta wing having auxiliary variable-sweep outboard panels /

Luoma, Arvo A.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 11).Mode of access: Internet

Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule /

Palmer, William E.
Braslow, Albert L.
Howell, Robert R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"July 20, 1956."Includes bibliographical references (p. 11).Mode of access: Internet

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).Mode of access: Internet

Effects of a sweptback hydrofoil on the force and longitudinal stability characteristics of a typical high-speed airplane /

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

January 1948

"December 2, 1948."Includes bibliographical references (p. 7).Mode of access: Internet

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics in ground effect of a large-scale model with a high disk-loading lifting fan mounted in the fuselage

deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

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

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).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

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

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items