Active filters
Displaying 1-50 of 105 results
Active control systems for load alleviation, flutter suppression and ride control.
Book/Text
[Neuilly sur Seine, North Atlantic Treaty Organization, 1974]
1974
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberVDS (AGARDograph, no. 175) no. 175-178 (1974) | Item locationOffsite |
Aerodynamic theory and its application to flutter. Prepared for Structures and Materials Panel of Advisory Group for Aeronautical Research and Development, Washington, D. C., April 1956.
Microform
Washington, National Advisory Committee for Aeronautics [1956]
1956
0 resources
Design procedures for flutter-free surface panels / Robert M. Laurenson and J. I. McPherson.
Book/Text
Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1977.
1977
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberJSF 84-855 | Item locationOffsite |
Flutter of blade rows with mistuning and structural coupling / par Hinne Bloemhof.
Book/Text
Lausanne : EPFL, 1988.
1988
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberJSD 96-314 | Item locationOffsite |
Massbalancing of aircraft control surfaces.
Book/Text
London, Chapman & Hall, 1954.
1954
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberVDY (Templeton, H. Massbalancing of aircraft control surfaces) | Item locationOffsite |
Introduction to the study of aircraft vibration and flutter [by] Robert H. Scanlan [and] Robert Rosenbaum.
Book/Text
New York, Macmillan [1951]
1951
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberVDYN (Scanlan, R. H. Introduction to the study of aircraft vibration and flutter. 1951) | Item locationOffsite |
Introduction to the study of aircraft vibration and flutter [by] Robert H. Scanlan [and] Robert Rosenbaum.
Book/Text
New York, Dover Publications [1968]
1968-1951
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberVDYN (Scanlan, R. H. Introduction to the study of aircraft vibration and flutter. 1968) | Item locationOffsite |
Theory and practice of flutter calucations for systems with many degrees of freedom.
Book/Text
Leiden [1952]
1952
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberVDYN+ (Vooren, A. I. van. de. Theory and practice of flutter calculations) | Item locationOffsite |
Planform curvature effects on flutter characteristics of a wing with 56⁰ leading-edge sweep and panel aspect ratio of 1.14 [microform] / Donald F. Keller and Maynard C. Sandford, Theresa L. Pinkerton.
Microform
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
1991
0 resources
Modal interaction in linear dynamic systems near degenerate modes [microform] / D. Afolabi.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
0 resources
User's guide to a system of finite-element supersonic panel flutter programs [microform] / Christine L. Woolley and John T. Batina.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
0 resources
Aeroelastic modal characteristics of mistuned blade assemblies [microform] : mode localization and loss of Eigenstructure / Christophe Pierre, Durbha V. Murthy.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
0 resources
An analytical and experimental study to investigate flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
Microform
[Washington, DC : National Aeronautics and Space Administration, 1991]
1991
0 resources
Flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
1991
0 resources
Pressure wave propagation studies for oscillating cascades [microform] / Dennis L. Huff.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter [microform] / Aparjit J. Mahajan and Krishna Rao V. Kaza.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Design and experimental validation of a flutter suppression controller for the active flexible wing [microform] / Martin R. Waszak, S. Srinathkumar.
Microform
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
1992
0 resources
Time simulation of flutter with large stiffness changes [microform] / Mordechay Karpel and Carol D. Wieseman.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Flutter suppression digital control law desighn and testing for the AFW wind-tunnel model [microform] / Vivek Mukhopadhyay.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Rolling maneuver load alleviation using active controls [microform] / Jessica A. Woods-Vedeler and Anthony S. Pototzky.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
An analytical and experimental investigation of flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Design, test, and evaluation of three active flutter suppression controllers [microform] / William M. Adams, Jr. ... [et al.].
Microform
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
1992
0 resources
Active flutter suppression using "dipole" filters [microform] / S. Srinathkumar, Martin R. Waszak.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Pressure measurements on a rectangular wing with a NACA0012 airfoil during conventional flutter [microform] / José A. Rivera, Jr. ... [et al.].
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods [microform] / E. Nissim.
Microform
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
1990
0 resources
An analytical and experimental investigation of flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
NACA0012 benchmark model using experimental flutter results with unsteady pressure distributions [microform] / José A. Rivera, Jr. ... [et al.].
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Hypersonic panel flutter in a rarefied atmosphere [microform] / Hugo B. Resende.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
A method of predicting quasi-steady aerodynamics for flutter analysis of high speed vehicles using steady CFD calculations [microform] / Robert C. Scott and Anthony S. Pototzky.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Laser velocimeter measurements of the flow field generated by a forward-swept propfan during flutter [microfilm] / Gary G. Podboy and Martin J. Krupar.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Ground vibration and flight flutter tests of the single-seat F-16XL aircraft with a modified wing [microform] / David F. Voracek.
Microform
Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
1993
0 resources
Flutter analysis using transversality theory [microform] / D. Afolabi.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Blade row interaction effects on flutter and forced response [microform] / Daniel H. Buffum.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
On curve veering and flutter of rotating blades [microform] / Daré Afolabi and Oral Mehmed.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Improvement of method for experimental determination of flutter speed by parameter indentification [microform] : final report / E. Nimbus.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Effects of spoiler surfaces on the aeroelastic behavior of a low-spect-ratio rectangular wing [microform] / Stanley R. Cole.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Flutter analysis of a supersonic cascade in time domain using an ADI Euler solver [microform] / T.S.R. Reddy and M.A. Bakhle and D.L. Huff.
Microform
[Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Unsteady hybrid vortex technique for transonic vortex flows and flutter applications [microform] / by Osama A. Kandil, principal investigator.
Microform
Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
1986
0 resources
An application of Eigenspace methods to symmetric flutter suppression [microform] / Robert E. Fennell.
Microform
Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Modern wing flutter analysis by computational fluid dynamics methods [microform] / Herbert J. Cunningham, John T. Batina, Robert M. Bennett.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I [microform] / Michael W. Kehoe.
Microform
Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service], 1987.
1987
0 resources
Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations [microform] / by Donald F. Keller and Ellen Parker Bullock.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
1991
0 resources
Remote pivot decoupler pylon [microform] : wing/store flutter suppressor.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1985]
1985
0 resources
Real-time flutter analysis [microform] / Robert Walker and Naren Gupta ; prepared for Ames Research Center, Dryden Flight Research Facility.
Microform
Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1984]
1984
0 resources
Method for experimental determination of flutter speed by parameter identification [microform] / E. Nissim and Glenn B. Gilyard.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989.
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60135Flutter clearance of the F-14A variable-sweep transition flight experiment airplane [microform] : phase 2 / Lawrence C. Freudinger and Michael W. Kehoe.
Microform
Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS65724Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods [microform] / Lawrence C. Freudinger.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1989.
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS72241The predicted effect of aerodynamic detuning of coupled bending-torsion unstalled supersonic flutter [microform] / Daniel Hoyniak and Sanford Fleeter.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
0 resources
Body-freedom flutter of a 1/2 scale forward-swept-wing-model, an experimental and analytical study [microform] / Richard Chipman, ... [et al.].
Microform
Bethpage, N.Y. : Grumman Aerospace Corporation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS88328Design and fabrication of the NASA decoupler pylon for the F-16 aircraft [microform] / J.D. Clayton, R.L. Haller, and J. M. Hassler, Jr.
Microform
Fort Worth, Tex. : General Dynamics, Fort Worth Division ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS88338No results found from Digital Research Books Beta
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