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Experimental Investigation Of Laminar Heat Transfer Characteristics Of A Manned Lifting Entry Vehicle At A Mach Number Of 20
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Book Synopsis Experimental Investigation of Laminar Heat- Transfer Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 20 by :
Download or read book Experimental Investigation of Laminar Heat- Transfer Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 20 written by and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Developing and Flight Testing the HL-10 Lifting Body by : Robert W. Kempel
Download or read book Developing and Flight Testing the HL-10 Lifting Body written by Robert W. Kempel and published by . This book was released on 1994 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 19.7 by :
Download or read book Longitudinal Aerodynamic Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 19.7 written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation at a Mach Number of 3.11 of the Lift, Drag, and Pitching-moment Characteristics of Five Blunt Lifting Bodies by : William Letko
Download or read book Experimental Investigation at a Mach Number of 3.11 of the Lift, Drag, and Pitching-moment Characteristics of Five Blunt Lifting Bodies written by William Letko and published by . This book was released on 1960 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 by : Davis H. Crawford
Download or read book Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 written by Davis H. Crawford and published by . This book was released on 1956 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt: At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.
Book Synopsis Stability Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 20.3 Helium by :
Download or read book Stability Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 20.3 Helium written by and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Flight Characteristics of a Model of the HL-10 Manned Lifting Entry Vehicle by : George M. Ware
Download or read book Investigation of the Flight Characteristics of a Model of the HL-10 Manned Lifting Entry Vehicle written by George M. Ware and published by . This book was released on 1967 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made of the low-subsonic flight characteristics of a model of the HL-10 manned lifting entry vehicle. This model was tested with two different center fins and with the larger center fin in combination with fin tips.
Book Synopsis Stability and Control Characteristics of a Manned Lifting Entry Vehicle at Mach Numbers from 2.29 to 4.63 by :
Download or read book Stability and Control Characteristics of a Manned Lifting Entry Vehicle at Mach Numbers from 2.29 to 4.63 written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Summary of an Advanced Manned Lifting Entry Vehicle Study by :
Download or read book Summary of an Advanced Manned Lifting Entry Vehicle Study written by and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Characteristics of a Manned Lifting Entry Vehicle with Various Fins at Mach Numbers from 1.50 to 2.86 by :
Download or read book Stability Characteristics of a Manned Lifting Entry Vehicle with Various Fins at Mach Numbers from 1.50 to 2.86 written by and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Heat-transfer Distributions on a Blunt Lifting Body at Mach 3.71 by : Robert L. Stallings
Download or read book Experimental Heat-transfer Distributions on a Blunt Lifting Body at Mach 3.71 written by Robert L. Stallings and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: The composite body consisted of a spherical nose segment, a delta-slab upper surface with blunt leading edges, wedge sides, and a conical lower surface. The tests were conducted both with and without roughness on the model for a range of angle of attack up to 400. Included is a complete tabulation of the experimental heatii rates and a discussion of the more significant findings.
Book Synopsis Investigation of the Heat Transfer to the HL-10 Manned Lifting Entry Vehicle at a Mach Number of 8 by :
Download or read book Investigation of the Heat Transfer to the HL-10 Manned Lifting Entry Vehicle at a Mach Number of 8 written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Investigation of Heat Transfer to an Unswept Cylinder Subjected to an Incident Shock and Flow Interference from an Upstream Body at Mach Numbers Up to 5.50 by : Howard S. Carter
Download or read book Free-flight Investigation of Heat Transfer to an Unswept Cylinder Subjected to an Incident Shock and Flow Interference from an Upstream Body at Mach Numbers Up to 5.50 written by Howard S. Carter and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer rates have been measured in free flight along the stagnation line of an unswept cylinder mounted transversely on an axial cylinder so that the shock wave from the hemispherical nose of the axial cylinder intersected the bow shock of the unswept transverse cylinder. Data were obtained at Mach numbers from 2.53 to 5.50 and at Reynolds numbers based on the transverse cylinder diameter from 1.00 x 106 to 1.87 x 106. Shadowgraph pictures made in a wind tunnel showed that the flow field was influenced by boundary-layer separation on the axial cylinder and by end effects on the transverse cylinder as well as by the intersecting shocks. Under these conditions, the measured heat-transfer rates had inconsistent variations both in magnitude and distribution which precluded separating the effects of these disturbances. The general magnitude of the measured heating rates at Mach numbers up to 3 was from 0.1 to 0.5 of the theoretical laminar heating rates along the stagnation line for an infinite unswept cylinder in undisturbed flow. At Mach numbers above 4 the measured heating rates were from 1.5 to 2 times the theoretical rates.
Book Synopsis Stability and Control Characteristics from Mach Number 1.50 to 2.86 of a Model of a Manned Lifting Entry Vehicle by :
Download or read book Stability and Control Characteristics from Mach Number 1.50 to 2.86 of a Model of a Manned Lifting Entry Vehicle written by and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Laminar Heat Transfer with Nonuniform Surface Temperature at M by : D.G. DeCoursin
Download or read book Experimental Investigation of Laminar Heat Transfer with Nonuniform Surface Temperature at M written by D.G. DeCoursin and published by . This book was released on 1959 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Heat Transfer Through Laminar and Turbulent Boundary Layers on a Cooled Flat Plate at a Mach Number of 2.4 by : Ellis G. Slack
Download or read book Experimental Investigation of Heat Transfer Through Laminar and Turbulent Boundary Layers on a Cooled Flat Plate at a Mach Number of 2.4 written by Ellis G. Slack and published by . This book was released on 1952 with total page 734 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests of the heat-transfer characteristics for laminar and turbulent boundary layers on a cooled flat plate were conducted at a Mach number of 2.4. Data were obtained for a Reynolds number range of 150.000 to 3,000.000 and for a surface-temperature range of -40 degrees F to 45 degrees F with recovery temperature of the order of 65 degrees F. The temperature-recovery factors agreed well with previous flat-plate reslts. The heat-transfer results were obtained with negative temperature gradients along the surface and, when related to the constant-surface-temperature case, were, in general, in good agreement with theory.
Book Synopsis Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration by : Charles B. Rumsey
Download or read book Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration written by Charles B. Rumsey and published by . This book was released on 1955 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
