Active filters
Displaying 1-50 of 58 results
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control [microform] / Scott C. Asbury and Craig A. Hunter.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
The control system for the X-33 linear aerospike engine [microform] / Jerry E. Jackson, Erich Espenschied, Jeffrey Klop.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Optimal pitch thrust-vector angle and benefits for all flight regimes [microform] / Glenn B. Gilyard, Alexander Bolonkin.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]
2000
0 resources
Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept [microform] / David J. Wing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
STOVL Control Integration Program [microform] / C. Weiss, P. McDowell and S. Watts.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
High-Alpha Research Vehicle (HARV) longitudinal controller : design, analyses, and simulation results [microform] / Aaron J. Ostroff, Keith D. Hoffler, Melissa S. Proffitt.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.
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
Xenon ion propulsion for orbit transfer [microform] / V.K. Rawlin, M.J. Patterson, and R.P. Gruber.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Design and evaluation of thrust vectored nozzles using a multicomponent thrust stand [microform] : final progress report, 10-01-88 - 01-31-90 / Thomas W. Carpenter, principal investigator ... [et al.].
Text
San Luis Obispo, Calif. : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Fourth High Alpha Conference, NASA Dryden Flight Research Center, Edwards, California, July 12-14, 1994 [microform]
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], 1994.
1994
0 resources
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Design of power electronics for TVC & EMA systems [microform] ; final report / R. Mark Nelms, J. Brett Bell, and Michael T. Shepherd.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels [microform] / Milton Lamb.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows [microform] / by Scott T. Imlay.
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
An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques [microform] : final report / by William G. Schweikhard and Werachone N. Singnoi.
Text
Lawrence, Kan. : University of Kansas ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
1995
0 resources
The performance evaluation of a jet flap on an advanced supersonic harrier [microform] : final report / principal investigators, Larry Dean Lipers, Doral R. Sandlin.
Text
San Luis Obispo, Calif. : California Polytechnic State University, Astronautical Engineering Dept. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
1984
0 resources
Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0̊ to 70̊ [microform] / Scott C. Asbury and Francis J. Capone.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1995]
1995
0 resources
Design specification for a thrust-vectoring, actuated-nose-strake flight control law for the high-alpha research vehicle [microform] / Barton J. Bacon ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle [microform] / W. Thomas Bundick ... [et al].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
HARV ANSER flight test data retrieval and processing procedures [microform] / Jessie C. Yeager.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
An experimental/modeling study of jet attachment during counterflow thrust vectoring [microform] : final report, NASA/NAG1-1736, grant period 1 July, 1995 - 30 June, 1996 / principal investigator, Paul J. Strykowski.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Integrated control using the SOFFT control structure [microform] : under contract NAS1-20185 / Nesim Halyo.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplane [microform] / Frank W. Burcham, Jr. ... [et al.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
1996
0 resources
An overview of the NASA F-18 High Alpha Research Vehicle [microform] / Albion H. Bowers ... [et al.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
1996
0 resources
Design and integration of an actuated nose strake control system [microform] / Bradley C. Flick ... [et al.].
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
1996
0 resources
Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Electro-mechanical actuator [microform] : DC resonant link controller / Kenneth E. Schreiner.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Flight testing the X-36--the test pilot's perspective [microform] / Laurence A. Walker.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
1997
0 resources
A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT [microform] / Patrick C. Murphy and John B. Davidson.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
High-alpha research vehicle lateral-directional control law description, analyses, and simulation results [microform] / John B. Davidson ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft [microform] / Martin J. Brenner.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
1996
0 resources
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane [microform] / Frederick J. Lallman, John B. Davidson, and Patrick C. Murphy.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.
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
Relative control effectiveness technique with application to airplane control coordination [microform] / Frederick J. Lallman.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service,] 1985.
1985
0 resources
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles [microform] / Mary L. Mason and Bobby L. Berrier.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
1985
0 resources
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.
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
Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap [microform] / Richard J. Re and Laurence D. Leavitt.
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
Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability [microform] / Linda S. Bangert and Laurence D. Leavitt.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS60139Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel [microform] / Albert L. Johns, ... [et al.].
Text
[Cleveland, Ohio : Lewis Research Center, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS62061Electromechanical actuation for thrust vector control applications [microform] / Mary Ellen Roth ; prepared for the National Aerospace and Electronics Conference (NAECON) sponsored by the Institute of Electrical and Electronics Engineers, Dayton, Ohio, May 21-25, 1990.
Text
[Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS66770Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring" [microform] : June 11, 1989-December 10, 1989 / by J.B. Tseng and C. Edward Lan.
Text
Lawrence, Kan. : Flight Research Laboratory, University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS69319Propulsion and control propellers with thruster nozzles primarily for aircraft applications [microform] / W. Pabst.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1986]
1986
0 resources
Solid rocket booster thrust vector control subsystem description [microform] / compiled by John Redmon, Jr.
Text
[ Huntsville, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1983]
1983
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS98999Noise generated by a flight weight, air flow control valve in a vertical takeoff and landing aircraft thrust vectoring system [microform] / Ronald G. Huff.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1989]
1989
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS105621Pressure measurements of impinging jet with asymmetric nozzle : progress report / principal investigator: Ho, Chih-Ming.
Text
Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988]
1988
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS112097Pressure measurements of impinging jet with asymmetric nozzle [microform] : progress report / principal investigator: Ho, Chih-Ming.
Text
Los Angeles, Calif. : Dept. of Aerospace Engineering, University of Southern California ; Hampton, VA : NASA Langley Research Center, [1988]
1988
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS112097No 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