A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form /

Division of aerodynamic loads on a semispan tilting-ducted-propeller model in hovering and transition flight. : Kalman J. Grunwald and Kenneth W. Goodson.

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical reference...

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...

An integral rquation relating the general time-dependent lift and downwash distributions on finite wings in subsonic flow

Drischler, Joseph A.
United States. National Aeronautics and Space Administration.

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

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails /

Peterson, Victor L.
Menees, Gene P.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referenc...

A method for calculating the aerodynamic forces due to arbitrary, time dependent downwash for a class of thin, flexible wings at supersonic speeds /

Warner, Robert W.
Packard, Barbara B.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flow, supersonic; Loads, aeroelasticity; Vibration and flutter.Includes ...

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

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

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

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

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

Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity /

Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

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

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Stroud, W. Jefferson.
Stein, Manuel.
Dexter, Cornelia B.
United States. National Aeronautics and Space Administration.

January 1971

"December 1971."Cover title.Includes bibliographical references (p. 136-137).Mode of access: Interne...

A comparison at mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizonatl tail heights behind a wing with 45 degrees of sweepback /

Stephenson, Jack D.
Bandettini, Angelo joint author.
Selan, Ralph joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "June 28, 1955."Includes bibliographical references: p. 16.Mode of access: Internet

Division of aerodynamic loads on a semispan tilting-ducted-propeller model in hovering and transition flight. : Kalman J. Grunwald and Kenneth W. Goodson.

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical reference...

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...

An integral rquation relating the general time-dependent lift and downwash distributions on finite wings in subsonic flow

Drischler, Joseph A.
United States. National Aeronautics and Space Administration.

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

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails /

Peterson, Victor L.
Menees, Gene P.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referenc...

A method for calculating the aerodynamic forces due to arbitrary, time dependent downwash for a class of thin, flexible wings at supersonic speeds /

Warner, Robert W.
Packard, Barbara B.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flow, supersonic; Loads, aeroelasticity; Vibration and flutter.Includes ...

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

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

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

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

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

Aerodynamic characteristics of a four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity /

Grunwald, Kalman J.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographica...

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

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Stroud, W. Jefferson.
Stein, Manuel.
Dexter, Cornelia B.
United States. National Aeronautics and Space Administration.

January 1971

"December 1971."Cover title.Includes bibliographical references (p. 136-137).Mode of access: Interne...

A comparison at mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizonatl tail heights behind a wing with 45 degrees of sweepback /

Stephenson, Jack D.
Bandettini, Angelo joint author.
Selan, Ralph joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "June 28, 1955."Includes bibliographical references: p. 16.Mode of access: Internet

Division of aerodynamic loads on a semispan tilting-ducted-propeller model in hovering and transition flight. : Kalman J. Grunwald and Kenneth W. Goodson.

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical reference...

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...

An integral rquation relating the general time-dependent lift and downwash distributions on finite wings in subsonic flow

Drischler, Joseph A.
United States. National Aeronautics and Space Administration.

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

A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form /

Abstract

Extracted data

A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form /

Abstract

Extracted data

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