An Introduction To Thrust Vectored Aircraft Nozzles

Author : David J. Wing
Publisher :
ISBN 13 :
Total Pages : 214 pages
Book Rating : 4.11/5 ( download)

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Download or read book Static Investigation of Two Fluidic Thrust-vectoring Concepts on a Two-dimensional Convergent-divergent Nozzle written by David J. Wing and published by . This book was released on 1994 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722936518
Total Pages : 128 pages
Book Rating : 4.17/5 ( download)

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Download or read book An Experimental Investigation of Thrust Vectoring Two-Dimensional Convergent-Divergent Nozzles Installed in a Twin-Engine Fighter Model at High Angles of Attack written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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...

Author : David J. Wing
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.42/5 ( download)

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Download or read book Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities written by David J. Wing and published by . This book was released on 1992 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : David J. Wing
Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.03/5 ( download)

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Download or read book Static Performance Investigation of a Skewed-throat Multiaxis Thrust-vectoring Nozzle Concept written by David J. Wing and published by . This book was released on 1994 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Steven A. Johnson
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.71/5 ( download)

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Download or read book Aircraft Ground Tests and Subscale Model Results of Axial Thrust Loss Caused by Thrust Vectoring Using Turning Vanes written by Steven A. Johnson and published by . This book was released on 1992 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : John S. Orme
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.62/5 ( download)

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Download or read book Initial Flight Test Evaluation of the F-15 ACTIVE Axisymmetric Vectoring Nozzle Performance written by John S. Orme and published by . This book was released on 1998 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: A full envelope database of a thrust-vectoring axisymmetric nozzle perfomance for the Pratt & Whitney Pitch/Yaw Balance Beam Nozzle (P/YBBN) is being developed using the F-15 Advanced Control Technology for Integrated Vehicles (ACTIVE) aircraft. At this time, flight research has been completed for steady-state pitch vector angles up to 20 deg. at an altitude of 30,000 ft from low power settings to maximum afterburner power. The nozzle performance database includes vector forces, internal nozzle pressures, and temperatures all of which can be used for regression analysis modeling. The database was used to substantiate a set of nozzle performance data from wind tunnel testing and computational fluid dynamic analyses. Findings from initial flight research at Mach 0.9 and 1.2 are presented in this paper. The results show that vector efficiency is strongly influenced by power setting. A significant discrepancy in nozzle performance has been discovered between predicted and measured results during vectoring.

Author : Robert J. Foley
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.41/5 ( download)

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Download or read book Static Thrust-vectoring Performance of Nonaxisymmetric Convergent-divergent Nozzles with Post-exit Yaw Vanes written by Robert J. Foley and published by . This book was released on 1991 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Laurence D. Leavitt
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.48/5 ( download)

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Download or read book Static Internal Performance of a Single-engine Nonaxisymmetric-nozzle Vaned-thrust-reverser Design with Thrust Modulation Capabilities written by Laurence D. Leavitt and published by . This book was released on 1985 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Richard J. Re
Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.42/5 ( download)

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Download or read book Static Internal Performance of Single Expansion-ramp Nozzles with Thrust Vectoring and Reversing written by Richard J. Re and published by . This book was released on 1982 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Benjamin Gal-Or
Publisher : Springer Science & Business Media
ISBN 13 : 1461389615
Total Pages : 277 pages
Book Rating : 4.13/5 ( download)

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Download or read book Vectored Propulsion, Supermaneuverability and Robot Aircraft written by Benjamin Gal-Or and published by Springer Science & Business Media. This book was released on 2013-11-09 with total page 277 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is designed to fill a professional vacuum in the new field of advance, high-angle, vectored stealth aircraft. The subject matter presented in the volume has never before been investigated and presented as a unified field of study because it covers entirely new fields and because specialized fragments of this unified field are scattered throughout literature in specific problems. The book is of interest to aeronautical and mechanical engineers, electrical and control engineers, aerospace industry, USAF, US Navy, NASA, pilots and instructors.