Research Catalog
New! Try our Article Search to discover online journals, books, and more from home with your library card.
Displaying 1-50 of 105 results
Active control systems for load alleviation, flutter suppression and ride control.
- Text
- [Neuilly sur Seine, North Atlantic Treaty Organization, 1974]
- 1974
- 1 Item
Item details Format Call Number Item Location Text VDS (AGARDograph, no. 175) no. 175-178 (1974) Offsite 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.
- Text
- Washington, National Advisory Committee for Aeronautics [1956]
- 1956
Design procedures for flutter-free surface panels / Robert M. Laurenson and J. I. McPherson.
- Text
- Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1977.
- 1977
- 1 Item
Item details Format Call Number Item Location Text JSF 84-855 Offsite Flutter of blade rows with mistuning and structural coupling / par Hinne Bloemhof.
- Text
- Lausanne : EPFL, 1988.
- 1988
- 1 Item
Item details Format Call Number Item Location Text JSD 96-314 Offsite Massbalancing of aircraft control surfaces.
- Text
- London, Chapman & Hall, 1954.
- 1954
- 1 Item
Item details Format Call Number Item Location Text VDY (Templeton, H. Massbalancing of aircraft control surfaces) Offsite Introduction to the study of aircraft vibration and flutter [by] Robert H. Scanlan [and] Robert Rosenbaum.
- Text
- New York, Macmillan [1951]
- 1951
- 1 Item
Item details Format Call Number Item Location Text VDYN (Scanlan, R. H. Introduction to the study of aircraft vibration and flutter. 1951) Offsite Introduction to the study of aircraft vibration and flutter [by] Robert H. Scanlan [and] Robert Rosenbaum.
- Text
- New York, Dover Publications [1968]
- 1968-1951
- 1 Item
Item details Format Call Number Item Location Text VDYN (Scanlan, R. H. Introduction to the study of aircraft vibration and flutter. 1968) Offsite Theory and practice of flutter calucations for systems with many degrees of freedom.
- Text
- Leiden [1952]
- 1952
- 1 Item
Item details Format Call Number Item Location Text VDYN+ (Vooren, A. I. van. de. Theory and practice of flutter calculations) Offsite 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.
- Text
- [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
Modal interaction in linear dynamic systems near degenerate modes [microform] / D. Afolabi.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
- 1991
User's guide to a system of finite-element supersonic panel flutter programs [microform] / Christine L. Woolley and John T. Batina.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
- 1991
Aeroelastic modal characteristics of mistuned blade assemblies [microform] : mode localization and loss of Eigenstructure / Christophe Pierre, Durbha V. Murthy.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
- 1991
An analytical and experimental study to investigate flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
- Text
- [Washington, DC : National Aeronautics and Space Administration, 1991]
- 1991
Flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
- 1991
Pressure wave propagation studies for oscillating cascades [microform] / Dennis L. Huff.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter [microform] / Aparjit J. Mahajan and Krishna Rao V. Kaza.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Design and experimental validation of a flutter suppression controller for the active flexible wing [microform] / Martin R. Waszak, S. Srinathkumar.
- Text
- [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
Time simulation of flutter with large stiffness changes [microform] / Mordechay Karpel and Carol D. Wieseman.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Flutter suppression digital control law desighn and testing for the AFW wind-tunnel model [microform] / Vivek Mukhopadhyay.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Rolling maneuver load alleviation using active controls [microform] / Jessica A. Woods-Vedeler and Anthony S. Pototzky.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
An analytical and experimental investigation of flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Design, test, and evaluation of three active flutter suppression controllers [microform] / William M. Adams, Jr. ... [et al.].
- Text
- [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
Active flutter suppression using "dipole" filters [microform] / S. Srinathkumar, Martin R. Waszak.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Pressure measurements on a rectangular wing with a NACA0012 airfoil during conventional flutter [microform] / José A. Rivera, Jr. ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
- 1992
Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods [microform] / E. Nissim.
- Text
- [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
An analytical and experimental investigation of flutter suppression via piezoelectric actuation [microform] / Jennifer Heeg.
- Text
- [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
NACA0012 benchmark model using experimental flutter results with unsteady pressure distributions [microform] / José A. Rivera, Jr. ... [et al.].
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
- 1992
Hypersonic panel flutter in a rarefied atmosphere [microform] / Hugo B. Resende.
- Text
- [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
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.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Laser velocimeter measurements of the flow field generated by a forward-swept propfan during flutter [microfilm] / Gary G. Podboy and Martin J. Krupar.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Ground vibration and flight flutter tests of the single-seat F-16XL aircraft with a modified wing [microform] / David F. Voracek.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
- 1993
Flutter analysis using transversality theory [microform] / D. Afolabi.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Blade row interaction effects on flutter and forced response [microform] / Daniel H. Buffum.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
On curve veering and flutter of rotating blades [microform] / Daré Afolabi and Oral Mehmed.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Improvement of method for experimental determination of flutter speed by parameter indentification [microform] : final report / E. Nimbus.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Effects of spoiler surfaces on the aeroelastic behavior of a low-spect-ratio rectangular wing [microform] / Stanley R. Cole.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
- 1990
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.
- Text
- [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
- 1992
Unsteady hybrid vortex technique for transonic vortex flows and flutter applications [microform] / by Osama A. Kandil, principal investigator.
- Text
- Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
- 1986
An application of Eigenspace methods to symmetric flutter suppression [microform] / Robert E. Fennell.
- Text
- Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
- 1988
Modern wing flutter analysis by computational fluid dynamics methods [microform] / Herbert J. Cunningham, John T. Batina, Robert M. Bennett.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
- 1988
Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I [microform] / Michael W. Kehoe.
- Text
- 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
Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations [microform] / by Donald F. Keller and Ellen Parker Bullock.
- Text
- [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
Remote pivot decoupler pylon [microform] : wing/store flutter suppressor.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration, 1985]
- 1985
Real-time flutter analysis [microform] / Robert Walker and Naren Gupta ; prepared for Ames Research Center, Dryden Flight Research Facility.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1984]
- 1984
Method for experimental determination of flutter speed by parameter identification [microform] / E. Nissim and Glenn B. Gilyard.
- Text
- [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.
- Text
- 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.
- Text
- [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.
- Text
- [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
- 1986
Body-freedom flutter of a 1/2 scale forward-swept-wing-model, an experimental and analytical study [microform] / Richard Chipman, ... [et al.].
- Text
- 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.
- Text
- 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/LPS88338
No results found from Digital Research Books Beta
Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.
