Books on the topic 'Thrust Vectoring Control (TVC)'

Nunn, R. H. TVC jet vane thermal modeling using parametric system identification. Monterey, Calif: Naval Postgraduate School, 1988.

Asbury, Scott C. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. Hampton, Va: Langley Research Center, 1993.

Lallman, Frederick J. Preliminary design study of a lateral-directional control system using thrust vectoring. [s.l.]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1985.

Mason, Mary L. A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle. Hampton, Va: Langley Research Center, 1992.

Nelms, R. M. Design of power electronics for TVC & EMA systems: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.

Capone, Francis J. Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Imlay, Scott T. Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows. Hampton, Va: Langley Research Center, 1986.

Wing, David J. Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability. Washington, D.C: National Aeronautics and Space Administration, 1997.

Foley, Robert J. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. Hampton, Va: Langley Research Center, 1991.

Asbury, Scott C. Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg. Hampton, Va: Langley Research Center, 1995.

Johnson, Steven A. A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Asbury, Scott C. Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: NASA, Dryden Flight Research Center, 1997.

Iliff, Kenneth W. Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Iliff, Kenneth W. Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Thomas, Carpenter, and Dryden Flight Research Facility, eds. Thrust vectoring for lateral-directional stability. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

Dulke, Michael F. Heat transfer modeling of jet vane Thrust Vector Control (TVC) Systems. 1987.

C, Asbury Scott, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

L, Mason Mary, and Langley Research Center, eds. Multiaxis aircraft control power from thrust vectoring at high angles of attack. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, ed. Preliminary design study of a lateral-directional control system using thrust vectoring. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

W, Pahle Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Thrust vectoring on the NASA F-18 high alpha research vehicle. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

W, Pahle Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Thrust vectoring on the NASA F-18 high alpha research vehicle. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

1935-, Lan C. Edward, and United States. National Aeronautics and Space Administration., eds. Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring": June 11, 1989-December 10, 1989. Lawrence, Kan: Flight Research Laboratory, University of Kansas Center for Research, 1989.

Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

J, Capone Francis, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Center, Langley Research, ed. Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Ann, Bare E., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

L, Berrier Bobby, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. and Langley Research Center, eds. Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

L, Mills Charles T., Mason Mary L, and Langley Research Center, eds. Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

R, Burley James, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, Davidson John, Murphy Patrick C, and Langley Research Center, eds. A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

B, Davidson John, Murphy Patrick C, and Langley Research Center, eds. A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

D, Leavitt Laurence, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

C, Pendergraft Odis, and Langley Research Center, eds. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

C, Pendergraft Odis, and Langley Research Center, eds. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

J, Bacon Barton, and Langley Research Center, eds. Design specification for a thrust-vectoring, actuated-nose-strake flight control law for the high-alpha research vehicle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Center, Langley Research, ed. Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

J, Capone Francis, and Langley Research Center, eds. Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.