An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack

An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 128

Get Book Here

Book Description


An Experimental Investigation of Thrust Vectoring Two-dimensional Covergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack

An Experimental Investigation of Thrust Vectoring Two-dimensional Covergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack PDF Author: Francis J. Capone
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 128

Get Book Here

Book Description


An Experimental Investigation of Thrust Vectoring Two-Dimensional Convergent-Divergent Nozzles Installed in a Twin-Engine Fighter Model at High Angles of Attack

An Experimental Investigation of Thrust Vectoring Two-Dimensional Convergent-Divergent Nozzles Installed in a Twin-Engine Fighter Model at High Angles of Attack PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722936518
Category :
Languages : en
Pages : 128

Get Book Here

Book Description
An investigation was conducted in the Langley 16-Foot Transonic Tunnel to determine thrust vectoring capability of subscale 2-D convergent-divergent exhaust nozzles installed on a twin engine general research fighter model. Pitch thrust vectoring was accomplished by downward rotation of nozzle upper and lower flaps. The effects of nozzle sidewall cutback were studied for both unvectored and pitch vectored nozzles. A single cutback sidewall was employed for yaw thrust vectoring. This investigation was conducted at Mach numbers ranging from 0 to 1.20 and at angles of attack from -2 to 35 deg. High pressure air was used to simulate jet exhaust and provide values of nozzle pressure ratio up to 9. Capone, Francis J. and Mason, Mary L. and Leavitt, Laurence D. Langley Research Center AIRCRAFT ENGINES; CONVERGENT-DIVERGENT NOZZLES; FIGHTER AIRCRAFT; LONGITUDINAL CONTROL; THRUST VECTOR CONTROL; ANGLE OF ATTACK; FLAPS (CONTROL SURFACES); JET EXHAUST; NOZZLE GEOMETRY; PRESSURE RATIO; RESEARCH AIRCRAFT; WIND TUNNEL TESTS; YAW...

NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 424

Get Book Here

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 180

Get Book Here

Book Description


Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept

Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept PDF Author: David J. Wing
Publisher:
ISBN:
Category :
Languages : en
Pages : 132

Get Book Here

Book Description


Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities

Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities PDF Author: David J. Wing
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 88

Get Book Here

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 740

Get Book Here

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 362

Get Book Here

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1300

Get Book Here

Book Description