A User's Guide to the Langley 16-Foot Transonic Tunnel Complex. Revision 1

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781723501678
Total Pages : 244 pages
Book Rating : 4.5/5 (16 download)

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Book Synopsis A User's Guide to the Langley 16-Foot Transonic Tunnel Complex. Revision 1 by : National Aeronautics and Space Administration (NASA)

Download or read book A User's Guide to the Langley 16-Foot Transonic Tunnel Complex. Revision 1 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-23 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt: The operational characteristics and equipment associated with the Langley 16-foot transonic tunnel complex which is located in buildings 1146 and 1234 at the Langley Research Center are described in detail. This complex consists of the 16-foot transonic wind tunnel, the static test facility, and the 16- by 24-inch water tunnel research facilities. The 16-foot transonic tunnel is a single-return atmospheric wind tunnel with a 15.5 foot diameter test section and a Mach number capability from 0.20 to 1.30. The emphasis for research conducted in this research complex is on the integration of the propulsion system into advanced aircraft concepts. In the past, the primary focus has been on the integration of nozzles and empennage into the afterbody of fighter aircraft. During the last several years this experimental research has been expanded to include developing the fundamental data base necessary to verify new theoretical concepts, inlet integration into fighter aircraft, nozzle integration for supersonic and hypersonic transports, nacelle/pylon/wing integration for subsonic transport configurations, and the study of vortical flows (in the 16- by 24-inch water tunnel). The purpose here is to provide a comprehensive description of the operational characteristics of the research facilities of the 16-foot transonic tunnel complex and their associated systems and equipments. Langley Research Center NASA-TM-102750, NAS 1.15:102750 RTOP 505-61-86-06...

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 994 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 994 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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Publisher :
ISBN 13 :
Total Pages : 218 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1995 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental and Computational Investigation of a Translating-Throat Single-Expansion-Ramp Nozzle

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental and Computational Investigation of a Translating-Throat Single-Expansion-Ramp Nozzle by : Karen A. Deere

Download or read book Experimental and Computational Investigation of a Translating-Throat Single-Expansion-Ramp Nozzle written by Karen A. Deere and published by . This book was released on 1999 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static performance of six innovative thrust reverser concepts for subsonic transport applications summary of the NASA Langley Innovative Thrust Reverser Test Program

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Publisher : DIANE Publishing
ISBN 13 : 1428996435
Total Pages : 369 pages
Book Rating : 4.4/5 (289 download)

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Book Synopsis Static performance of six innovative thrust reverser concepts for subsonic transport applications summary of the NASA Langley Innovative Thrust Reverser Test Program by :

Download or read book Static performance of six innovative thrust reverser concepts for subsonic transport applications summary of the NASA Langley Innovative Thrust Reverser Test Program written by and published by DIANE Publishing. This book was released on 2000 with total page 369 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Isolated Performance at Mach Numbers From 0.60 to 2.86 of Several Expendable Nozzle Concepts for Supersonic Applications

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ISBN 13 :
Total Pages : 202 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Isolated Performance at Mach Numbers From 0.60 to 2.86 of Several Expendable Nozzle Concepts for Supersonic Applications by : Richard J. Re

Download or read book Isolated Performance at Mach Numbers From 0.60 to 2.86 of Several Expendable Nozzle Concepts for Supersonic Applications written by Richard J. Re and published by . This book was released on 2001 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt: Investigations have been conducted in the Langley 16-Foot Transonic Tunnel (at Mach numbers from 0.60 to 1.25) and in the Langley Unitary Plan Winf Tunnel (at Mach numbers from 2.16 to 2.86) at an angle of attack of O° to determine the isolated performane of several expendable nozzle concepts for supersonic noaugmented turbojet applications. The effects of centerbody base shape, shroud length, shroud ventilation, cruciform shroud expansion ration, and cruciform shroud flap vectoring were investigated. The nozzle pressure ration range, which was a function of Mach number, was between 1.9 and 11.8 in the 16-Foot Transonic Tunnel and between 7.9 and 54.9 in the Unitary Plan WInd Tunnel. Discharge coefficient, thrust-minus-drag, and the forces and moments generated by vectoring the divergent shroud flaps (for Mach numbers of 0.60 to 1.25 only) of a cruciform nozzle configuration were measured.

Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers

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ISBN 13 :
Total Pages : 272 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers by : Linda S. Bangert

Download or read book Effect of Afterbody Geometry on Aerodynamic Characteristics of Isolated Nonaxisymmetric Afterbodies at Transonic Mach Numbers written by Linda S. Bangert and published by . This book was released on 1992 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Convoluted Divergent Flap Contouring on the Performance of a Fixed-Geometry Nonaxisymmetric Exhaust Nozzle

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effects of Convoluted Divergent Flap Contouring on the Performance of a Fixed-Geometry Nonaxisymmetric Exhaust Nozzle by : Scott C. Asbury

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Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control

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ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control by : Scott C. Asbury

Download or read book Static Performance of a Fixed-Geometry Exhaust Nozzle Incorporating Porous Cavities for Shock-Boundary Layer Interaction Control written by Scott C. Asbury and published by . This book was released on 1999 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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ISBN 13 :
Total Pages : 424 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Paper by : United States. National Aeronautics and Space Administration

Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1990 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Static Performance of a Cruciform Nozzle with Multiaxis Thrust-vectoring and Reverse-thrust Capabilities by : David J. Wing

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:

Installation Effects of Wing-mounted Turbofan Nacelle-pylons on a 1/17 Scale, Twin-engine, Low-wing Transport Model

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ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Installation Effects of Wing-mounted Turbofan Nacelle-pylons on a 1/17 Scale, Twin-engine, Low-wing Transport Model by :

Download or read book Installation Effects of Wing-mounted Turbofan Nacelle-pylons on a 1/17 Scale, Twin-engine, Low-wing Transport Model written by and published by . This book was released on 1992 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Investigation of Two Fluidic Thrust-vectoring Concepts on a Two-dimensional Convergent-divergent Nozzle

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ISBN 13 :
Total Pages : 214 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Static Investigation of Two Fluidic Thrust-vectoring Concepts on a Two-dimensional Convergent-divergent Nozzle by : David J. Wing

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:

Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds

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ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds by : John R. Carlson

Download or read book Two-dimensional Converging-diverging Rippled Nozzles at Transonic Speeds written by John R. Carlson and published by . This book was released on 1994 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Static Investigation of the Thrust Vectoring System of the F/A-18 High-alpha Research Vehicle

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ISBN 13 :
Total Pages : 172 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Static Investigation of the Thrust Vectoring System of the F/A-18 High-alpha Research Vehicle by : Mary L. Mason

Download or read book A Static Investigation of the Thrust Vectoring System of the F/A-18 High-alpha Research Vehicle written by Mary L. Mason and published by . This book was released on 1992 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2

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ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2 by : E. Ann Bare

Download or read book Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2 written by E. Ann Bare and published by . This book was released on 1992 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 136 pages
Book Rating : 4.:/5 (319 download)

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Download or read book NASA Technical Memorandum written by and published by . This book was released on 1992 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: