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Experimental Investigation Of A 10 Degrees Conical Turbojet Plug Nozzle With Translating Primary And Secondary Shrouds At Mach Numbers From 0 To 20
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Book Synopsis Experimental Investigation of a 10 Deg Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0 by : Donald L. Bresnahan
Download or read book Experimental Investigation of a 10 Deg Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0 written by Donald L. Bresnahan and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of a 10 Degrees Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0 by : Donald L. Bresnahan
Download or read book Experimental Investigation of a 10 Degrees Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0 written by Donald L. Bresnahan and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of a 10 Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0 by : Donald L. Bresnahan
Download or read book Experimental Investigation of a 10 Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0 written by Donald L. Bresnahan and published by . This book was released on 1969 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis EXPERIMENTAL INVESTIGATION OF A 10 PER CENT CONICAL TURBOJET PLUG NOZZLE WITH TRANSLATING PRIMARY AND SECONDARY SHROUDS AT MACH NUMBERS FROM O TO 2.0 by : UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION.
Download or read book EXPERIMENTAL INVESTIGATION OF A 10 PER CENT CONICAL TURBOJET PLUG NOZZLE WITH TRANSLATING PRIMARY AND SECONDARY SHROUDS AT MACH NUMBERS FROM O TO 2.0 written by UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. and published by . This book was released on 1965 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of a 10 Conical Turbojet Plug Nozzle with IRIS Primary and Translating Shroud at Mach Numbers from 0 to 2.0 by : Donald L. Bresnahan
Download or read book Experimental Investigation of a 10 Conical Turbojet Plug Nozzle with IRIS Primary and Translating Shroud at Mach Numbers from 0 to 2.0 written by Donald L. Bresnahan and published by . This book was released on 1968 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the Lewis Research Center's nozzle static test facility and the 8 by 6 foot supersonic wind tunnel to determine the performance characteristics of a 10 half-angle conical turbojet plug nozzle wih a simutated iris primary throat and overall design pressure ratio of 26.3.
Book Synopsis Performance of a 10° Conical Plug Nozzle with Various Primary Flap and Nacelle Configurations at Mach Numbers from 0 to 1.97 by : Douglas E. Harrington
Download or read book Performance of a 10° Conical Plug Nozzle with Various Primary Flap and Nacelle Configurations at Mach Numbers from 0 to 1.97 written by Douglas E. Harrington and published by . This book was released on 1970 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index by :
Download or read book Government Reports Annual Index written by and published by . This book was released on 1969 with total page 938 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of a 10 Deg Conical Plug Nozzle with a Stowed Thrust Reverser at Mach Numbers from 0 to 2.0 by : Fred W. Steffen
Download or read book Performance of a 10 Deg Conical Plug Nozzle with a Stowed Thrust Reverser at Mach Numbers from 0 to 2.0 written by Fred W. Steffen and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Heat-transfer Characteristics of a Film-cooled Plug Nozzle with Translating Shroud by : Francis C. Chenoweth
Download or read book Experimental Investigation of Heat-transfer Characteristics of a Film-cooled Plug Nozzle with Translating Shroud written by Francis C. Chenoweth and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer characteristics of film cooled plug nozzle with translating shroud.
Book Synopsis Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source by : Albert L. Johns
Download or read book Quiescent-air Performance of a Truncated Turbojet Plug Nozzle with Shroud and Plug Base Flows from a Common Source written by Albert L. Johns and published by . This book was released on 1969 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Coolant Flow Effects on the Performance of a Conical Plug Nozzle at Mach Numbers from 0 to 2.0 by :
Download or read book Coolant Flow Effects on the Performance of a Conical Plug Nozzle at Mach Numbers from 0 to 2.0 written by and published by . This book was released on 1970 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Performance of a 10 Conical Plug Nozzle with a Stowed Thrust Reverser at Mach Numbers from 0 to 2.0 by : Fred W. Steffen
Download or read book Performance of a 10 Conical Plug Nozzle with a Stowed Thrust Reverser at Mach Numbers from 0 to 2.0 written by Fred W. Steffen and published by . This book was released on 1970 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Investigation of Installation Effects on a Plug Nozzle with a Series of Boattailed Primary Shrouds Installed on an Underwing Nacelle by : Verlon L. Head
Download or read book Flight Investigation of Installation Effects on a Plug Nozzle with a Series of Boattailed Primary Shrouds Installed on an Underwing Nacelle written by Verlon L. Head and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Several variations of a boattailed shroud for a 10 deg conical plug nozzle were tested using an F-106B aircraft for Mach 0.6 to 1.3. The data were obtained so that the tradeoff between boattail and plug size could be studied for an underwing nacelle location. The nozzles were tested with J85-GE-13 turbojet engine, and the data were compared to previous flight results of installed plug nozzles. Boattail area varied from 31 to 66 percent of the nacelle area. The effect of increasing projected boattail area was to increase the gross thrust coefficient in the same way as from isolated data for flight Mach numbers below 0.85. The highest gross thrust coefficient (0.958) was obtained at Mach 0.95 with a long circular arc shroud configuration with a very small amount of secondary air flow.
Book Synopsis Performance Characteristics of a 10 Deg Conical Plug Nozzle at Mach Numbers Up to 1 29 by :
Download or read book Performance Characteristics of a 10 Deg Conical Plug Nozzle at Mach Numbers Up to 1 29 written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Performance of a 10° Conical Plug Nozzle with a Multispoke Primary and Translating External Shroud by : Donald L. Bresnahan
Download or read book Internal Performance of a 10° Conical Plug Nozzle with a Multispoke Primary and Translating External Shroud written by Donald L. Bresnahan and published by . This book was released on 1972 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer Characteristics of Partially Film Coded Plug Nozzle on a J-85 Afterburning Turbojet Engine by : Stanley M. Nosek
Download or read book Heat-transfer Characteristics of Partially Film Coded Plug Nozzle on a J-85 Afterburning Turbojet Engine written by Stanley M. Nosek and published by . This book was released on 1976 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: Plug nozzle film cooling data were obtained downstream of a slot located at 42 percent of the total plug length on a J-85 engine. Film cooling reduced the aft end wall temperature as much as 150 K, reduced total pressure loss in the upstream convection cooling passages by 50 percent, and reduced estimated compressor bleed flow requirement by 14 percent compared to an all convectively cooled nozzle. Shock waves along the plug surface strongly influenced temperature distributions on both convection and film cooled portions. The effect was most severe at nozzle pressure ratios below 10 where adverse pressure gradients were most severe.
Book Synopsis Pandex Current Index to Scientific and Technical Literature by :
Download or read book Pandex Current Index to Scientific and Technical Literature written by and published by . This book was released on 1969 with total page 932 pages. Available in PDF, EPUB and Kindle. Book excerpt:
