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Effect of control surface mass unbalance on the stability of a closed-loop active control system [microform] / E. Nissim.

Text

[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1989.

1989

0 resources

Satellite-matrix-switched, time-division-multiple-access network simulator [microform] / William D. Ivancic ... [et al.].

Text

1989

0 resources

The use of the Regier number in the structural design with flutter constraints [microform] / H.J. Dunn and Robert V. Doggett, Jr.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Optical measurement of unducted fan flutter [microform] / Anatole P. Kurkov and Oral Mehmed.

Text

[Washington, DC] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1991]

1991

0 resources

Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model [microform] / J.E. Turnberg.

Text

[Windsor Locks, CT] : Hamilton Standard Division, United Technologies Corp. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1986]

1986

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

Aeroelasticity of wing and wing-body configurations on parallel computers [microform] / Chansup Byun.

Text

San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

1995

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

Research and applications in structures at the NASA Langley Research Center [microform] / Irving Abel.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Aeroelastic calculations using CFD for a typical business jet model [microform] / Michael D. Gibbons.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1996]

1996

0 resources

ASTROP2 users manual [microform] : a program for aeroelastic stability analysis of propfans / T.S.R. Reddy and John M. Lucero.

Text

[Washington, DC] : National Aeronautics and Space Administration ; [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

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

Sensitivity analysis of flutter response of a wing incorporating finite-span corrections [microform] / Jason C. Issac, Rakesh K. Kapania, and J.-F. M. Barthelemy.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]

1994

0 resources

Final technical report for aeroelastic analysis of turbomachinery for space propulsion [microform] : NASA grant number NAG3-1449, grant duration--January 13, 1993 to February 23, 1996 / Theo G. Keith, Jr. & Durbha V. Murthy.

Text

Toledo, Ohio : Dept. of Mechanical, Industrial and Manufacturing Engineering, University of Toledo ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

1996

0 resources

Overview of recent flight flutter testing research at NASA Dryden [microform] / Martin J. Brenner, Richard C. Lind, and David F. Voracek.

Text

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.

1997

0 resources

Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation.

Text

Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

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

Final technical report for aeroelastic analysis of counter rotation fans [microform] : NASA grant number NAG3-742; grant duration, September 1, 1986 to December 31, 1993 / Theo G. Keith, Jr., principal investigator; Durbha V. Murthy, co-principal investigator.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

User's guide for MSAP2D [microform] : a program for unsteady aerodynamic and aeroelastic (flutter and forced response) analysis of multistage compressors and turbines : under grant NAG3-1137 / T.S.R. Reddy and R. Srivastava.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]

1996

0 resources

Correlation filtering of modal dynamics using the Laplace wavelet [microform] / Lawrence C. Freudinger, Rick Lind, and Martin J. Brenner.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Improved flight test procedures for flutter clearance [microform] / Rick C. Lind, Martin J. Brenner, and Lawrence C. Freudinger.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations [microform] : NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996 / Theo G. Keith, Jr., principal investigator; Rakesh Srivastava, co-principal investigator.

Text

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

1997

0 resources

Response of the alliance 1 proof-of-concept airplane under gust loads [microform] / A.S. Naser, A.S. Pototsky, and C.V. Spain ; [prepared ... under contract NAS1-96014].

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]

2001

0 resources

MAVRIC flutter model transonic limit cycle oscillation test [microform] / John W. Edwards ... [et al.].

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 required

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

0 resources

Application of a linearized unsteady aerodynamic analysis to standard cascade configurations [microform] / Joseph M. Verdon and William J. Usab, Jr.

Text

[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.

1986

0 resources

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/LPS60135

Flutter 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/LPS65724

Digital-flutter-suppression-system investigations for the active flexible wing wind-tunnel model [microform] / Boyd Perry III ... [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/LPS69415

Using 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/LPS69438

Flutter 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/LPS72241

Ground vibration test of an F-16 airplane with modified decoupler pylons [microform] / F.W. Cazier, Jr., M.W. Kehoe.

Text

Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.

1986

1 resource

Available online

http://purl.access.gpo.gov/GPO/LPS85478

Design 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

Analytical flutter investigation of a composite propfan model [microform] / K.R.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/LPS92391

An aeroelastician's perspective of wind tunnel and flight experiences with active control of structural response and stability [microform] / Perry W. Hanson.

Text

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]

1984

1 resource

Available online

http://purl.access.gpo.gov/GPO/LPS95400

Vibration and flutter of mistuned bladed-disk assemblies [microform] / Krishna Rao V. Kaza and Robert E. Kielb.

Text

[Washington, D.C. : National Aeronautics and Space Administration, 1984]

1984

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

Aeroelastic analyses of the SemiSpan Supersonic Transport (S⁴T) wind tunnel model at Mach 0.95 / Jiyoung Hur.

Text

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2014.

2013-7

1 resource

Available online

https://purl.fdlp.gov/GPO/gpo53309

Nonlinear aeroelastic analysis of the HIAD TPS coupon in the NASA 8' high temperature tunnel : theory and experiment / Benjamin D. Goldman, Robert C. Scott, Earl H. Dowell.

Text

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2014.

2014-5

1 resource

Available online

https://purl.fdlp.gov/GPO/gpo53628

Overview of recent flight flutter testing research at NASA Dryden / Martin J. Brenner, Richard C. Lind, and David F. Voracek.

Text

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, April 1997.

1997-4

1 resource

Available online

https://purl.fdlp.gov/GPO/gpo65710

ASTROP2 users manual : a program for aeroelastic stability analysis of propfans / T.S.R. Reddy and John M. Lucero.

Text

Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, March 1996.

1996-3

1 resource

Available online

https://purl.fdlp.gov/GPO/gpo66479

MAVRIC flutter model transonic limit cycle oscillation test / John W. Edwards [and four others].

Text

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2001.

2001-5

1 resource

Available online

https://purl.fdlp.gov/GPO/LPS22880

Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer / Shantaram S. Pai, David S. Riha.

Text

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]

2013

1 resource

Available online

https://purl.fdlp.gov/GPO/gpo40538

Analysis of an unswept propfan blade with a semiempirical dynamic stall model / T.S.R. Reddy, K.R.V. Kaza.

Text

Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, January 1989.

1989-1

1 resource

Available online

Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / Aparajit J. Mahajan [and three others].

Text

Washington, D.C. : NASA, April 1992.

1992-4

1 resource

Available online

Flying beyond flutter with the X-56A aircraft / Jacob Schaefer [and nine others].

Text

Edwards, California : National Aeronautics and Space Administration, Armstrong Flight Research Center, March 2023.

2023-3

1 resource

Available online

Special course on unsteady aerodynamics.

Text

Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1980.

1980

1 item

Format	Call number	Item location
FormatBook/Text	Call numberAGARD-R-679	Item locationOff-site

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Displaying 48 of 48 results

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