Author: John Gordon Taylor
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 108
Book Description
Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability
Author: John Gordon Taylor
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 108
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 108
Book Description
Static Investigation of a Two-dimensional Convergent-divergent Nozzle with Simultaneous Pitch and Yaw Thrust Vectoring
Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability
Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities
Author: David J. Wing
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 88
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 88
Book Description
Static Performance of a Cruciform Nozzle with Multiaxis Thrust-Vectoring and Reverse-Thrust Capabilities
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722771683
Category :
Languages : en
Pages : 82
Book Description
A multiaxis thrust vectoring nozzle designed to have equal flow turning capability in pitch and yaw was conceived and experimentally tested for internal, static performance. The cruciform-shaped convergent-divergent nozzle turned the flow for thrust vectoring by deflecting the divergent surfaces of the nozzle, called flaps. Methods for eliminating physical interference between pitch and yaw flaps at the larger multiaxis deflection angles was studied. These methods included restricting the pitch flaps from the path of the yaw flaps and shifting the flow path at the throat off the nozzle centerline to permit larger pitch-flap deflections without interfering with the operation of the yaw flaps. Two flap widths were tested at both dry and afterburning settings. Vertical and reverse thrust configurations at dry power were also tested. Comparison with two dimensional convergent-divergent nozzles showed lower but still competitive thrust performance and thrust vectoring capability. Wing, David J. and Asbury, Scott C. Langley Research Center...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722771683
Category :
Languages : en
Pages : 82
Book Description
A multiaxis thrust vectoring nozzle designed to have equal flow turning capability in pitch and yaw was conceived and experimentally tested for internal, static performance. The cruciform-shaped convergent-divergent nozzle turned the flow for thrust vectoring by deflecting the divergent surfaces of the nozzle, called flaps. Methods for eliminating physical interference between pitch and yaw flaps at the larger multiaxis deflection angles was studied. These methods included restricting the pitch flaps from the path of the yaw flaps and shifting the flow path at the throat off the nozzle centerline to permit larger pitch-flap deflections without interfering with the operation of the yaw flaps. Two flap widths were tested at both dry and afterburning settings. Vertical and reverse thrust configurations at dry power were also tested. Comparison with two dimensional convergent-divergent nozzles showed lower but still competitive thrust performance and thrust vectoring capability. Wing, David J. and Asbury, Scott C. Langley Research Center...
An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack
Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept
Static Internal Performance of a Two-dimensional Convergent-divergent Nozzle with Thrust Vectoring
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 424
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 424
Book Description