Pressure wave propagation studies for oscillating cascades /Author: Huff, Dennis L.
Publisher: [Washington, DC] : National Aeronautics and Space Administration,
Date: [1992] This title can be found in 1 Iowa libraries.
Flutter analysis of a supersonic cascade in time domain using an ADI Euler solverFormat: [microform] /
Author: Reddy, T. S. R.
Publisher: [Washington, D.C.] : NASA ;
Date: 1992] This title can be found in 2 Iowa libraries.
Flutter suppression via piezoelectric actuation /Author: Heeg, Jennifer.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1991] This title can be found in 1 Iowa libraries.
User's guide to a system of finite-element supersonic panel flutter programs /Author: Woolley, Christine L.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1991] This title can be found in 1 Iowa libraries.
Modal interaction in linear dynamic systems near degenerate modes /Author: Afolabi, D.
Publisher: [Washington, DC] : National Aeronautics and Space Administration,
Date: [1991] This title can be found in 1 Iowa libraries.
Planform curvature effects on flutter characteristics of a wing with 56⁰ leading-edge sweep and panel aspect ratio of 1.14 /Author: Keller, Donald F.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,
Date: 1991. This title can be found in 1 Iowa libraries.
An analytical and experimental study to investigate flutter suppression via piezoelectric actuation /Author: Heeg, Jennifer.
Publisher: [Washington, DC] : [National Aeronautics and Space Administration],
Date: [1991] This title can be found in 1 Iowa libraries.
Aeroelastic modal characteristics of mistuned blade assemblies : mode localization and loss of Eigenstructure /Author: Pierre, Christophe,
Publisher: [Washington, DC] : National Aeronautics and Space Administration,
Date: [1991] This title can be found in 1 Iowa libraries.
Wund tunnel wall effects in a linear oscillating cascade /Author: Buffum, Daniel H.
Publisher: [Washington, DC] : National Aeronautics and Space Administration,
Date: [1991] This title can be found in 1 Iowa libraries.
An experimental study of tip shape effects on the flutter of aft-swept, flat-plate wings /Author: Dansberry, Bryan E.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1990. This title can be found in 1 Iowa libraries.
Effects of spoiler surfaces on the aeroelastic behavior of a low-spect-ratio rectangular wing /Author: Cole, Stanley R.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1990] This title can be found in 1 Iowa libraries.
Experimental transonic flutter characteristics of two 72 ̊-sweep delta-wing models /Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1989] This title can be found in 1 Iowa libraries.
Surface pressure distributions on a delta wing undergoing large amplitude pitching oscillations /Author: Thompson, Scott A.
Publisher: Notre Dame, Ind. : Department of Aerospace and Mechanical Engineering, University of Notre Dame,
Date: [1989] This title can be found in 1 Iowa libraries.
The effectiveness of vane-aileron excitation in the experimental determination of flutter speed by parameter identification /Author: Nissim, E.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1990. This title can be found in 1 Iowa libraries.
Aeroservoelastic wind-tunnel investigations using the active flexible wing model : status and recent accomplishments /Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1989] This title can be found in 1 Iowa libraries.
Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods /Author: Freudinger, Lawrence C.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1989. This title can be found in 1 Iowa libraries.
Flutter suppression control law synthesis for the active flexible wing model /Author: Mukhopadhyay, Vivek.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1989] This title can be found in 1 Iowa libraries.
Control surface spanwise placement in active flutter suppression systems /Author: Nissim, E.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division,
Date: 1988. This title can be found in 1 Iowa libraries.
Results of a parametric aeroelastic stability analysis of a generic x-wing aircraft /Author: Woods-Vedeler, Jessica A.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1989] This title can be found in 1 Iowa libraries.
Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 /Author: Rivera, José A.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1989. This title can be found in 1 Iowa libraries.
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