An application of a numerical technique to lifting-surface theory for calculation of unsteady aerodynamic forces due to continuous sinusoidal gusts on several wing planforms at subsonic speeds / Harold N. Murrow, Kermit G. Pratt and Joseph A Drischler.

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

Calculation of vortex lift effect for cambered wings by the suction analogy /

Lan, C. Edward (Chaun-Pau Edward), 1935-
Chang, Jen-Fu.
University of Kansas. Center for Research.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"July 1981"--Cover."The University of Kansas Center for Research, Inc."Includes bibliographical refe...

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 ...

AN APPLICATION OF A NUMERICAL TECHNIQUE TO LIFTING-SURFACE THEORY FOR CALCULATION OF UNSTEADY AERODYNAMIC FORCES DUE TO CONTINUOUS SINUSOIDAL GUSTS ON SEVERAL WING PLANFORMS AT SUBSONIC SPEEDS

Pratt, K. G.
Murrow, H. N.
Drischler, J. A.

February 1963

Numerical lifting-surface method to calculate direct gust forces and moments on wings at subsonic sp...

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 ...

A method for calculating the generalized aerodynamic forces on rectangular wings deforming symmetrically in supersonic flight with indicial or sinusoidal time dependence /

Bond, Rueben.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

A Simple method of estimating the subsonic lift and damping in roll of sweptback wings /

Polhamus, Edward C.
United States. National Advisory Committee for Aeronautics.

January 1949

A method of modifying existing correction factors of lifting-surface theory to account approximately...

Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds /

Harmon, Sidney M.
United States. National Advisory Committee for Aeronautics.

January 1951

A method utilizing source singularities is presented for obtaining the linearized downwash field due...

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

Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges /

Margolis, Kenneth.
Elliott, Miriam H.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and load...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust /

McFarland, Donald R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Fluid mechanics; Stability and control.Includes bib...

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

Cover title." April 1962."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles, Stabilit...

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

Calculation of vortex lift effect for cambered wings by the suction analogy /

Lan, C. Edward (Chaun-Pau Edward), 1935-
Chang, Jen-Fu.
University of Kansas. Center for Research.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"July 1981"--Cover."The University of Kansas Center for Research, Inc."Includes bibliographical refe...

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 ...

AN APPLICATION OF A NUMERICAL TECHNIQUE TO LIFTING-SURFACE THEORY FOR CALCULATION OF UNSTEADY AERODYNAMIC FORCES DUE TO CONTINUOUS SINUSOIDAL GUSTS ON SEVERAL WING PLANFORMS AT SUBSONIC SPEEDS

Pratt, K. G.
Murrow, H. N.
Drischler, J. A.

February 1963

Numerical lifting-surface method to calculate direct gust forces and moments on wings at subsonic sp...

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 ...

A method for calculating the generalized aerodynamic forces on rectangular wings deforming symmetrically in supersonic flight with indicial or sinusoidal time dependence /

Bond, Rueben.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

A Simple method of estimating the subsonic lift and damping in roll of sweptback wings /

Polhamus, Edward C.
United States. National Advisory Committee for Aeronautics.

January 1949

A method of modifying existing correction factors of lifting-surface theory to account approximately...

Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds /

Harmon, Sidney M.
United States. National Advisory Committee for Aeronautics.

January 1951

A method utilizing source singularities is presented for obtaining the linearized downwash field due...

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

Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges /

Margolis, Kenneth.
Elliott, Miriam H.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and load...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust /

McFarland, Donald R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Fluid mechanics; Stability and control.Includes bib...

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

Cover title." April 1962."Aerodynamics, aircraft;Aerodynamics, missiles and space vehicles, Stabilit...

Contribution to methods for calculating the flow about thin lifting wings at transonic speeds : Analytic expressions for the far field /

Klunker, E. B.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N72-11289.Cover title.Includes bibliographical references (p. 15...

Calculation of vortex lift effect for cambered wings by the suction analogy /

Lan, C. Edward (Chaun-Pau Edward), 1935-
Chang, Jen-Fu.
University of Kansas. Center for Research.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"July 1981"--Cover."The University of Kansas Center for Research, Inc."Includes bibliographical refe...

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 ...

An application of a numerical technique to lifting-surface theory for calculation of unsteady aerodynamic forces due to continuous sinusoidal gusts on several wing planforms at subsonic speeds / Harold N. Murrow, Kermit G. Pratt and Joseph A Drischler.

Abstract

Extracted data

An application of a numerical technique to lifting-surface theory for calculation of unsteady aerodynamic forces due to continuous sinusoidal gusts on several wing planforms at subsonic speeds / Harold N. Murrow, Kermit G. Pratt and Joseph A Drischler.

Abstract

Extracted data

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