A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils /

Steady inviscid transonic flows over planar airfoils : a search for a simplified procedure /

Magnus, R.
Yoshihara, H. (Hideo)
Ames Research Center.
General Dynamics Corporation. Convair Division.

January 1973

"Prepared by General Dynamics/Convair Aerospace Division ... for Ames Research Center."Cover title.B...

Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction /

Howlett, James T.
Langley Research Center.

January 1992

"June 1992"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. 13-14...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

A finite difference method for the solution of the transonic flow around harmonically oscillating wings /

Ehlers, F. Edward.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Aircraft Company ... for Langley Research Center."Cover title.Bibliog...

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Development of a nonlinear unsteady transonic flow theory /

Stahara, Stephen S.
Spreiter, John R.
Langley Research Center.
Nielsen Engineering & Research.

January 1973

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center."Cover title.Bibli...

The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings /

Ehlers, F. Edward, joint author.
Sebastian, James D., joint author.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Feb. 1978.Prepared for Langley Research Center under Contact NAS 1-14204.Includes bibliograph...

An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn.

Dunn, H. J., 1947-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Includes bibliographical references.Nov. 1980."Langley Research Center."Mode of access: Internet

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

A linear aerodynamic analysis for unsteady transonic cascades /

Verdon, Joseph M.
Caspar, Joseph R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

STAR category 02.Distributed to depository libraries in microfiche."September 1984"--Cover.Includes ...

Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings /

Weatherill, W. H.
Sebastian, James D.
Ehlers, F. Edward.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center.""December 1975....

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

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

Steady inviscid transonic flows over planar airfoils : a search for a simplified procedure /

Magnus, R.
Yoshihara, H. (Hideo)
Ames Research Center.
General Dynamics Corporation. Convair Division.

January 1973

"Prepared by General Dynamics/Convair Aerospace Division ... for Ames Research Center."Cover title.B...

Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction /

Howlett, James T.
Langley Research Center.

January 1992

"June 1992"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. 13-14...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

A finite difference method for the solution of the transonic flow around harmonically oscillating wings /

Ehlers, F. Edward.
Langley Research Center.
Boeing Commercial Airplane Company.

January 1974

"Prepared by Boeing Commercial Aircraft Company ... for Langley Research Center."Cover title.Bibliog...

Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /

Howlett, James T.
Bland, Samuel R.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Development of a nonlinear unsteady transonic flow theory /

Stahara, Stephen S.
Spreiter, John R.
Langley Research Center.
Nielsen Engineering & Research.

January 1973

"Prepared by Nielsen Engineering & Research, Inc. ... for Langley Research Center."Cover title.Bibli...

The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings /

Ehlers, F. Edward, joint author.
Sebastian, James D., joint author.
Boeing Commercial Airplane Company.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

Issued Feb. 1978.Prepared for Langley Research Center under Contact NAS 1-14204.Includes bibliograph...

An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn.

Dunn, H. J., 1947-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Includes bibliographical references.Nov. 1980."Langley Research Center."Mode of access: Internet

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

A linear aerodynamic analysis for unsteady transonic cascades /

Verdon, Joseph M.
Caspar, Joseph R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

STAR category 02.Distributed to depository libraries in microfiche."September 1984"--Cover.Includes ...

Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings /

Weatherill, W. H.
Sebastian, James D.
Ehlers, F. Edward.
Langley Research Center.
Boeing Commercial Airplane Company.

"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center.""December 1975....

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Chattot, J. J.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Aeromechanics Laboratory"--Cover.Includes bibliographical references.Mode of access: Inte...

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

Steady inviscid transonic flows over planar airfoils : a search for a simplified procedure /

Magnus, R.
Yoshihara, H. (Hideo)
Ames Research Center.
General Dynamics Corporation. Convair Division.

January 1973

"Prepared by General Dynamics/Convair Aerospace Division ... for Ames Research Center."Cover title.B...

Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction /

Howlett, James T.
Langley Research Center.

January 1992

"June 1992"--Cover.Prepared at Langley Research Center.Includes bibliographical references (p. 13-14...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils /

Abstract

Extracted data

A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils /

Abstract

Extracted data

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