Author: Mary L. MasonPublisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 84
Book Description
Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-vectoring Vanes
Author: Mary L. MasonPublisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 84
Book Description
Static Performance of Nonaxisymmetric Nozzles with Yaw Thrust-Vectoring Vanes
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722772338
Category :
Languages : en
Pages : 76
Book Description
A static test was conducted in the static test facility of the Langley 16 ft Transonic Tunnel to evaluate the effects of post exit vane vectoring on nonaxisymmetric nozzles. Three baseline nozzles were tested: an unvectored two dimensional convergent nozzle, an unvectored two dimensional convergent-divergent nozzle, and a pitch vectored two dimensional convergent-divergent nozzle. Each nozzle geometry was tested with 3 exit aspect ratios (exit width divided by exit height) of 1.5, 2.5 and 4.0. Two post exit yaw vanes were externally mounted on the nozzle sidewalls at the nozzle exit to generate yaw thrust vectoring. Vane deflection angle (0, -20 and -30 deg), vane planform and vane curvature were varied during the test. Results indicate that the post exit vane concept produced resultant yaw vector angles which were always smaller than the geometric yaw vector angle. Losses in resultant thrust ratio increased with the magnitude of resultant yaw vector angle. The widest post exit vane produced the largest degree of flow turning, but vane curvature had little effect on thrust vectoring. Pitch vectoring was independent of yaw vectoring, indicating that multiaxis thrust vectoring is feasible for the nozzle concepts tested. Mason, Mary L. and Berrier, Bobby L. Langley Research Center...
Static Thrust-vectoring Performance of Nonaxisymmetric Convergent-divergent Nozzles with Post-exit Yaw Vanes
Author: Robert J. FoleyPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 88
Book Description
NASA Technical Paper
Author: NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 424
Book Description
Static Performance of an Axisymmetric Nozzle with Post-exit Vanes for Multiaxis Thrust Vectoring
Author: Bobby L. BerrierPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1224
Book Description
Scientific and Technical Aerospace Reports
Author: NASA Scientific and Technical Publications
Author: Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1480
Book Description