Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5

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ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5 by : Earl A. Price (Jr.)

Download or read book Afterbody Drag Investigation of a Twin-nozzle Fighter-type Model at Mach Numbers from 0.6 to 1.5 written by Earl A. Price (Jr.) and published by . This book was released on 1972 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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

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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:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 562 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1976 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers

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ISBN 13 :
Total Pages : 182 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers by : Earl A. Price (Jr.)

Download or read book A Parametric Investigation of the Annular Jet Concept for Obtaining Afterbody Drag Data at Transonic Mach Numbers written by Earl A. Price (Jr.) and published by . This book was released on 1978 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Afterbody/nozzle Pressure Distributions of a Twin-tail Twin-engine Fighter with Axisymmetric Nozzles at Mach Numbers from 0.6 to 1.2

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Total Pages : 220 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Afterbody/nozzle Pressure Distributions of a Twin-tail Twin-engine Fighter with Axisymmetric Nozzles at Mach Numbers from 0.6 to 1.2 by : David J. Wing

Download or read book Afterbody/nozzle Pressure Distributions of a Twin-tail Twin-engine Fighter with Axisymmetric Nozzles at Mach Numbers from 0.6 to 1.2 written by David J. Wing and published by . This book was released on 1995 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.:/5 (31 download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1248 pages
Book Rating : 4.:/5 (89 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1984 with total page 1248 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalogue, United States Public Documents

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ISBN 13 :
Total Pages : 1252 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Monthly Catalogue, United States Public Documents by :

Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1984 with total page 1252 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Parametric Study of Afterbody/nozzle Drag on Twin Two-dimensional Convergent-divergent Nozzles at Mach Numbers from 0.60 to 1.20

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

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Book Synopsis Parametric Study of Afterbody/nozzle Drag on Twin Two-dimensional Convergent-divergent Nozzles at Mach Numbers from 0.60 to 1.20 by :

Download or read book Parametric Study of Afterbody/nozzle Drag on Twin Two-dimensional Convergent-divergent Nozzles at Mach Numbers from 0.60 to 1.20 written by and published by . This book was released on 1986 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

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ISBN 13 :
Total Pages : 484 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1978 with total page 484 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect on Empennage Location on Twin-engine Afterbody/nozzle Aerodynamic Characteristics at Mach Numbers from 0.6 to 1.2

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ISBN 13 :
Total Pages : 228 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect on Empennage Location on Twin-engine Afterbody/nozzle Aerodynamic Characteristics at Mach Numbers from 0.6 to 1.2 by : Laurence D. Leavitt

Download or read book Effect on Empennage Location on Twin-engine Afterbody/nozzle Aerodynamic Characteristics at Mach Numbers from 0.6 to 1.2 written by Laurence D. Leavitt and published by . This book was released on 1983 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 Deg

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 Deg by :

Download or read book Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 Deg written by and published by . This book was released on 1985 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 ̊

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 ̊ by : Laurence D. Leavitt

Download or read book Static Internal Performance of a Two-dimensional Convergent Nozzle with Thrust-vectoring Capability Up to 60 ̊ written by Laurence D. Leavitt and published by . This book was released on 1985 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 910 pages
Book Rating : 4.3/5 (91 download)

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Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 910 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Air Frame-propulsion Interference, Papers and Discussion of the Fluid Dynamics Panel Symposium Held at Rome..., 3-6 September 1974

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ISBN 13 :
Total Pages : 454 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Air Frame-propulsion Interference, Papers and Discussion of the Fluid Dynamics Panel Symposium Held at Rome..., 3-6 September 1974 by :

Download or read book Air Frame-propulsion Interference, Papers and Discussion of the Fluid Dynamics Panel Symposium Held at Rome..., 3-6 September 1974 written by and published by . This book was released on 1975 with total page 454 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:

Exhaust-nozzle Characteristics for a Twin-jet Variable-wing-sweep Fighter Airplane Model at Mach Numbers to 2.2

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ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Exhaust-nozzle Characteristics for a Twin-jet Variable-wing-sweep Fighter Airplane Model at Mach Numbers to 2.2 by : David E. Reubush

Download or read book Exhaust-nozzle Characteristics for a Twin-jet Variable-wing-sweep Fighter Airplane Model at Mach Numbers to 2.2 written by David E. Reubush and published by . This book was released on 1974 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: