Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 128
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 Covergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack
Author: Francis J. CaponePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 128
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
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722936518
Category :
Languages : en
Pages : 128
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
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 424
Book Description
NASA Technical Paper
Author: Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept
Author: David J. WingStatic Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities
Author: David J. WingPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 88
Book Description
Scientific and Technical Aerospace Reports
Author: NASA Technical Memorandum
Author: Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1300
Book Description