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Linearized unsteady aerodynamic analysis of the acoustic response to wake/blade-row interaction by Verdon, Joseph M.
[Cleveland, Ohio] : Hanover, Md. :; [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001Call Number: Loading…
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Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions by Verdon, Joseph M.
[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1990Call Number: Loading…
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3
A linear aerodynamic analysis for unsteady transonic cascades by Verdon, Joseph M.
[Washington, D.C.?] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984Call Number: Loading…
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Development of a linearized unsteady Euler analysis with application to wake/blade-row interactions by Verdon, Joseph M.
[Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999Call Number: Loading…
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5
Development of a linearized unsteady Euler analysis for turbomachinery blade rows by Verdon, Joseph M.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1995Call Number: Loading…
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6
Development of an unsteady aerodynamic analysis for finite-deflection subsonic cascades by Verdon, Joseph M.
Washington, D.C. : [Springfield, Va.] : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981Call Number: Loading…
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Development of a linearized unsteady aerodynamic analysis for cascade gust response predictions by Verdon, Joseph M.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990Call Number: Loading…
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8
A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows by Montgomery, Matthew D.
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996Other Authors: “…Verdon, Joseph M.…”
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A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows : under contract NAS3-26618 by Montgomery, Matthew D.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1997Other Authors: “…Verdon, Joseph M.…”
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10
Development of a steady potential solver for use with linearized, unsteady aerodynamic analyses by Hoyniak, Daniel
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1991Other Authors: “…Verdon, Joseph M.…”
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11
Development of unsteady aerodynamic analyses for turbomachinery aeroelastic and aeroacoustic applications
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1991Other Authors: “…Verdon, Joseph M.…”
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12
Active control of wake/blade-row interaction noise through the use of blade surface actuators by Kousen, Kenneth A.
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993Other Authors: “…Verdon, Joseph M.…”
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13
An analysis for high Reynolds number inviscid/viscid interactions in cascades by Barnett, M. (Mark)
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1993Other Authors: “…Verdon, Joseph M.…”
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Related Subjects
Cascades (Fluid dynamics)
Euler equations of motion
Mathematical models
Unsteady aerodynamics
Unsteady flow
Unsteady flow (Aerodynamics)
Aerodynamic characteristics
Gust loads
Three dimensional flow
Acoustics
Aerodynamic load
Aerodynamics
Aerodynamics, Transonic
Aeroelasticity
Airplanes
Annular ducts
Axial flow
Blades
Boundary conditions
Computational fluid dynamics
Computer programs
Design analysis
Differential equations
Euler analysis
Fan noise
Far fields
Finite volume method
Flutter (Aerodynamics)
Inviscid flow
Jet planes