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Base Heat Transfer Pressure Ratios And Configuration Effects Obtained On A 1 27 Scall Saturn C 1 Model At Mach Numbers From 01 To 20
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Book Synopsis Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Ratios and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Ratios and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Rations and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at MAch Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Rations and Configuration Effects Obtained on a 1/27 Scale Saturn (C-1) Model at MAch Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1963 with total page 1342 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Journal of the Royal Aeronautical Society by :
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1963 with total page 950 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1963 with total page 644 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5 by : Thorval Tendeland
Download or read book Effects of Mach Number and Wall-temperature Ratio on Turbulent Heat Transfer at Mach Numbers from 3 to 5 written by Thorval Tendeland and published by . This book was released on 1959 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The heat-transfer data obtained from the model were found to correlate when the T' method of Sommer and Short was used. The increase in turbulent heat-transfer rate with a reduction in wall to free-stream temperature ratio was of the same order of magnitude as has been found for the turbulent skin-friction coefficient.
Book Synopsis Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 by : J. David Dearing
Download or read book Laminar Heat-transfer Distributions for a Blunted-cone, Cone-frustum Reentry Configuration at Mach 10 written by J. David Dearing and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer to a Sphere with a Retrorocket Exhausting Into a Free Stream by : Robert A. Wasko
Download or read book Heat Transfer to a Sphere with a Retrorocket Exhausting Into a Free Stream written by Robert A. Wasko and published by . This book was released on 1962 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 by : Robert A. Wasko
Download or read book Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 written by Robert A. Wasko and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Base Heating with a 5.47-Percent Saturn SA-1 Booster Model at Mach Numbers 0.8 and 1.15 by : JOSEPH R. JR. PARKER
Download or read book An Investigation of Base Heating with a 5.47-Percent Saturn SA-1 Booster Model at Mach Numbers 0.8 and 1.15 written by JOSEPH R. JR. PARKER and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the base recirculation characteristics of the simulated propellant pump turbine exhaust gases of a 5.47-% scale model of the SA-1 Saturn afterbody. Gaseous hydrogen was used to simulate the combustible turbine exhaust gas of the fullscale missile. Base heating and pressure data were obtained at simulated flight trajectory conditions of M=0.8 0.8(16,000-ft) and M=1.15 1.15(27,500-ft) using several turbine exhaust duct configurations. In addition, the effect on base heating with one engine inoperative, of variation in turbine exhaust gas momen um, of finned-model operation, of variation in engine O/F ratio, and of variation in altitude was investigated. At both simulated flight trajectory conditions, the lowest base heating rates were obtained using a streamlined turbine exhaust duct configuration. The following conditions reduced base heating, based on data obtained with the long turbine exhaust ducts: operation with one engine inoperative, increased turbine exhaust gas discharge momentum, and increased engine O/F ratio. (Author).
Book Synopsis Variation in Heat Transfer During Transient Heation of a Hemisphere at a Mach Numer of 2 by : Roland D. English
Download or read book Variation in Heat Transfer During Transient Heation of a Hemisphere at a Mach Numer of 2 written by Roland D. English and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 by : Paige B. Burbank
Download or read book Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 written by Paige B. Burbank and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions at Mach Numbers of 6.0 and 9.6 Over Two Reentry Configurations for the Five-stage Scout Vehicle by : Paul F. Holloway
Download or read book Heat-transfer and Pressure Distributions at Mach Numbers of 6.0 and 9.6 Over Two Reentry Configurations for the Five-stage Scout Vehicle written by Paul F. Holloway and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 by : Ross B. Robinson
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Roughness on Heat Transfer to Hemisphere Cylinders at Mach Numbers 10.4 and 11.4 by : James C. Dunavant
Download or read book Effect of Roughness on Heat Transfer to Hemisphere Cylinders at Mach Numbers 10.4 and 11.4 written by James C. Dunavant and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
