Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116
Book Description
Static Internal Performance Including Thrust Vectoring and Reversing of Two-dimensional Convergent-divergent Nozzles
Static Internal Performance of a Thrust Vectoring and Reversing Two-dimensional Convergent-divergent Nozzle with an Aft Flap
Static Internal Performance Including Thrust Vectoring and Reversing of Tow-dimensional Convergent-divergent Nozzles
Author: Richard J. Re
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 116
Book Description
Static Internal Performance of a Thrust Vectoring and Reversing Two-dimensional Convergent-divergent Nozzle with an Aft Flap
Author: Richard J. Re
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 120
Book Description
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 120
Book Description
Static Internal Performance of a Two-dimensional Convergent-divergent Nozzle with Thrust Vectoring
Static Internal Performance of a Two-dimensional Convergent-divergent Nozzle with Thrust Vectoring
Author: E. Ann Bare
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 120
Book Description
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 120
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...
Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 600
NASA Technical Paper
Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 ̊
Author: Laurence D. Leavitt
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 76
Book Description