Active filters
Displaying 1-50 of 54 results
CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999 [microform] / edited by Woodrow Whitlow, Jr., Emily N. Todd ; proceedings of a workshop sponsored by the Confederation of European Aerospace Societies (CEAS), the American Institute of Aeronautics and Astronautics (AIAA), the National Aeronautics and Space Administration (NASA), Washington, D.C., and the Institute for Computer Applications in Science and Engineering (ICASE), Hampton, Virginia, and held in Williamsburg, Virginia, June 22-25, 1999.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1999]
1999
0 resources
Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver [microform] / T.S.R. Reddy and R. Srivastava, O. Mehmed.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : Available from National Technical Information Service, [1999]
1999
0 resources
Flutter analysis of supersonic axial flow cascades using a high resolution euler solver. Part 1, Formulation and validation [microform] / T.S.R. Reddy ... [et al.].
Text
Washington, DC : National Aeronautics and Space Administration, [1992]
1992
0 resources
Some observations on the Houbolt-Rainey and peak-hold methods of flutter onset prediction [microform] / Robert V. Doggett, Jr.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1989
0 resources
Shape sensitivity analysis of flutter response of a laminated wing [microform] / Fred D. Bergen and Rakesh K. Kapania.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, [1988]
1988
0 resources
Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model [microform] / José A. Rivera ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
1991
0 resources
Additional development of the XTRAN3S computer program [microform] / C.J. Borland.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
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
0 resources
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
0 resources
Flutter analysis of composite box beams [microform] / Matthew Greenman.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Improvements to the fastex flutter analysis computer code [microform] : final report, grant NAG 2-377 / Ronald F. Taylor.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
1987
0 resources
Development of flight testing techniques [microform] : final report, 10/31/79 - 10/31/84 / principal investigator, Doral R. Sandlin.
Text
San Luis Obispo, CA : Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
1984
0 resources
Flutter prediction for a wing with active aileron control [microform] : final report / principal investigators, Kevin Penning, Doral R. Sandlin.
Text
San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1983]
1983
0 resources
Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments [microform] / Robert V. Doggett, Jr., José A. Rivera, Jr., and Eric C. Stewart.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Experimental classical flutter results of a composite advanced turboprop model [microform] / O. Mehmed and K.R.V. Kaza.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum I [microform] / J.D. Clayton and R.L. Haller.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
1985
0 resources
Design and fabrication of the NASA decoupler pylon for the F-16 aircraft, addendum II [microform] / J.D. Clayton, R.L. Haller, and J.M. Hassler, Jr.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
1985
0 resources
FPCAS3D user's guide [microform] : full potential aeroelastic program / Milind A. Bakhle.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
An interactive software for conceptual wing flutter analysis and parametric study [microform] / Vivek Mukhopadhyay.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
A presentation on robust flutter margin analysis and a flutterometer [microform] / Rick C. Lind.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
X-38 vehicle 131 flutter assessment [microform] / James P. Smith.
Text
[Houston, Tex.] : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Methods for in-flight robustness evaluation [microform] : summary of research / James D. Paduano, Eric Feron, Marty Brenner.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A worst-case approach for on-line flutter prediction [microform] / Rick C. Lind and Martin J. Brenner.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Robust flutter margin analysis that incorporates flight data [microform] / Rick Lind, Martin J. Brenner.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Application of TURBO-AE to flutter prediction [microform] : aeroelastic code development / Daniel Hoyniak, Todd A. Simons ; [prepared under contract NAS3-27725 task 6 EDR-19540].
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
0 resources
Optimization of training sets for neural-net processing of characteristic patterns from vibrating solids [microform] / Arthur J. Decker.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredDeveloping uncertainty models for robust flutter analysis using ground vibration test data [microform] / Starr Potter and Rick Lind.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredA probabilistic approach to model update [microform] / Lucas G. Horta, Mercedes C. Reaves, David F. Voracek.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredFlow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances [microform] / Lisa J. Bjarke.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS59777The application of active controls technology to a generic hypersonic aircraft configuration [microform] / M.G. Gilbert ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS69437Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model [microform] / Walter A. Silva and Robert M. Bennett.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS69438Mass balancing of hollow fan blades [microform] / Robert E. Kielb.
Text
[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.].
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/LPS88328Analytical and experimental investigation of mistuning in propfan flutter [microform] / Krishna Rao V. Kaza ... [et al].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
1987
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS92416Viscous effects on transonic airfoil stability and response [microform] / H. M. Berry, J. T. Batina, T. Y. Yang.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Exploratory flutter test in a cryogenic wind tunnel [microform] / Stanley R. Cole.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Ground vibration test results for drones for aerodynamic and structural testing (DAST)/aeroelastic research wing (ARW-1R) aircraft [microform] / Timothy H. Cox and Glenn B. Gilyard.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1986]
1986
0 resources
Flutter of swept fan blades [microform] / Robert E. Kielb and K. R. V. Kaza.
Text
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
An airfoil flutter model suspension system to accomdate large static transonic airloads [microform] / Wilmer H. Reed, III.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
0 resources
Flutter analysis of the Shuttle tile overlay repair concept / Kim S. Bey ... [and others].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2007]
2007
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo4708Harmonic balance computations of fan aeroelastic stability / Milind A. Bakhle, T.S.R. Reddy ; prepared for the International Forum on Aeroelasticity and Structural Dynamics (IFASD 2009) cosponsored by CEAS and AIAA, Seattle, Washington, June 21-25, 2009.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
2010
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo6507Application of approximate unsteady aerodynamics for flutter analysis / Chan-gi Pak and Wesley W. Li.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center, [2010]
2010
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo11878Reduced uncertainties in the flutter analysis of the aerostructures test wing / Chan-gi Pak and Shun-fat Lung.
Text
Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
2011
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo13290An airfoil flutter model suspension system to accommodate large static transonic airloads / Wilmer H. Reed, III.
Text
Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
1985
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo21276Unsteady aerodynamic model tuning for precise flutter prediction / Chan-gi Pak.
Text
Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
2011
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo24034Basis function approximation of transonic aerodynamic influence coefficient matrix / Wesley W. Li and Chan-gi Pak.
Text
Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
2011
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo24037Modal filtering for control of flexible aircraft / Peter M. Suh, Dimitri N. Mavris.
Text
Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
2013-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo54680Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / Gregory P. Herrick.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2014.
2014-12
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo57922Re-computation of numerical results contained in NACA report no. 496 / Boyd Perry, III.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2015.
2015-6
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo60787An interactive software for conceptual wing flutter analysis and parametric study / Vivek Mukhopadhyay.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1996.
1996-8
1 resource
Available online
http://purl.fdlp.gov/GPO/gpo75891No results found from Digital Research Books Beta
Digital books for research from multiple sources worldwide - all free to read, download, and keep. No library card required.
Explore Digital Research Books Beta