Author: Bobby L. BerrierPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 136
Book Description
Internal Performance of Two Nozzles Utilizing Gimbal Concepts for Thrust Vectoring
Author: Bobby L. BerrierPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 136
Book Description
Internal Performance of Two Nozzles Utilizing Gimbal Concepts for Thrust Vectoring
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781723184185
Category :
Languages : en
Pages : 130
Book Description
The internal performance of an axisymmetric convergent-divergent nozzle and a nonaxisymmetric convergent-divergent nozzle, both of which utilized a gimbal type mechanism for thrust vectoring was evaluated in the Static Test Facility of the Langley 16-Foot Transonic Tunnel. The nonaxisymmetric nozzle used the gimbal concept for yaw thrust vectoring only; pitch thrust vectoring was accomplished by simultaneous deflection of the upper and lower divergent flaps. The model geometric parameters investigated were pitch vector angle for the axisymmetric nozzle and pitch vector angle, yaw vector angle, nozzle throat aspect ratio, and nozzle expansion ratio for the nonaxisymmetric nozzle. All tests were conducted with no external flow, and nozzle pressure ratio was varied from 2.0 to approximately 12.0. Berrier, Bobby L. and Taylor, John G. Langley Research Center CONVERGENT-DIVERGENT NOZZLES; GIMBALS; NOZZLE EFFICIENCY; NOZZLE GEOMETRY; THRUST VECTOR CONTROL; ASPECT RATIO; PERFORMANCE TESTS; PITCH (INCLINATION); WIND TUNNEL TESTS; YAW...
NASA Technical Paper
Author: NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 432
Book Description
NASA Technical Memorandum
Author: Scientific and Technical Aerospace Reports
Author: Internal Performance of a Nonaxisymmetric Nozzle with a Rotating Upper Flap and a Center-pivoted Lower Flap
Author: David J. WingPublisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 64
Book Description
Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept
Author: David J. WingNASA Scientific and Technical Publications
Author: A Static Investigation of the Thrust Vectoring System of the F/A-18 High-alpha Research Vehicle
Author: Mary L. MasonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 172
Book Description