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Aerodynamic Heating On The Corrugated Surface Of A 1020 Half Angle Blunted Cone At Mach 67
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Book Synopsis Aerodynamic Heating on the Corrugated Surface of a 10.20 Half-angle Blunted Cone at Mach 6.7 by : Irving Weinstein
Download or read book Aerodynamic Heating on the Corrugated Surface of a 10.20 Half-angle Blunted Cone at Mach 6.7 written by Irving Weinstein and published by . This book was released on 1981 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Heating on the Corrugated Surface of a 10.2° Half-angle Blunted Cone at Mach 6.7 by : Irving Weinstein
Download or read book Aerodynamic Heating on the Corrugated Surface of a 10.2° Half-angle Blunted Cone at Mach 6.7 written by Irving Weinstein and published by . This book was released on 1981 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow by : David E. Boylan
Download or read book Laminar Heat Transfer on Sharp and Blunt Ten-degree Cones in Conical and Parallel Low-density Flow written by David E. Boylan and published by . This book was released on 1973 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents heat-transfer-rate measurements on sharp and blunt 10-deg half-angle cones at angles of attack between -9 and +10 deg in a low-density, hypersonic wind tunnel. Circumferential and longitudinal distributions are presented for cold wall conditions for a range at Mach and Reynolds numbers. The effect of source-like flows was studied by utilizing both conical and contoured expansion nozzles with the same free-stream similarity parameters and model wall temperatures. Comparisons are made with previously published experimental and theoretical results. (Author).
Book Synopsis Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 by : Jerome D. Julius
Download or read book Measurements of Pressure and Local Heat Transfer on a 20° Cone at Angles of Attack Up to 20° for a Mach Number of 4.95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone During Free Flight at Mach Numbers Up to 20.8 by :
Download or read book Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone During Free Flight at Mach Numbers Up to 20.8 written by and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8 by : Benjamine J. Garland
Download or read book Measurements of Aerodynamic Heat Transfer in Turbulent Separated Regions at a Mach Number of 1.8 written by Benjamine J. Garland and published by . This book was released on 1958 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Convective Heat-transfer Rates on Large-scale Conical Bodies at Hypersonic Speeds by : David Alexander Stewart
Download or read book Convective Heat-transfer Rates on Large-scale Conical Bodies at Hypersonic Speeds written by David Alexander Stewart and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer rates were measured on large-angle conical bodies with large half-angles between 50 degrees and 90 degrees, at angles of attack from 0 degrees. The results at 0 degree angle of attack were predicted with Lees' similarity theory, using calculated flow properties at the boundary-layer edge. The calculated flow properties were obtained from Newtonian theory for the 50 degree cone and from a one- or two-strip solution using the method of integral relations for other cones. At 0 degree angle of attack, an increase in cone angle resulted in a decrease in the heating rate over much of the body. However, high heating rates occurred at the shoulder of the both the half-angle = 80 degree and half-angle =90 degree shapes because of local pressure gradients. On the windward side of the cones, the heating rate increased with angle of attack.
Book Synopsis Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4 by :
Download or read book Heat Transfer to a Hemispherically Blunted 9 Deg Half-angle Cone Cylinder at Hypersonic Free Flight Mach Numbers Up to 20.4 written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 by : Peter F. Intrieri
Download or read book Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 written by Peter F. Intrieri and published by . This book was released on 1962 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ by : Dennis M. Bushnell
Download or read book Heat-transfer and Pressure Distributions on Spherically Blunted 25 ̊half-angle Cone at Mach 8 and Angles of Attack Up to 90 ̊ written by Dennis M. Bushnell and published by . This book was released on 1968 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heating Rate Measurements Over 30 Deg and 40 Deg (half Angle) Blunt Cones in Air and Helium in the Langley Expansion Tube Facility by :
Download or read book Heating Rate Measurements Over 30 Deg and 40 Deg (half Angle) Blunt Cones in Air and Helium in the Langley Expansion Tube Facility written by and published by . This book was released on 1980 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Convective heat-transfer measurements were made on the conical portion of spherically blunted cones (30 deg and 40 deg half angle) in the Langley expansion tube. The test gases used were helium and air: flow velocities were about 6.8 km/sec for helium and about 5.1 km/sec for air. The measured heating rates were compared with calculated results using a viscous shock-layer computer code. For air, various techniques to determine flow velocity yielded nearly identical results, but for helium the flow velocity varied by as much as 8% depending on which technique was used. The measured heating rates were in satisfactory agreement with calculation for helium test gas if the higher flow velocity was used, but for air and for helium assuming the lower flow velocity, the measurements were significantly greater than theory and the discrepancy increased with increasing distance along the cone.
Book Synopsis Static Aerodynamic Characteristics of Three Blunted Sixty-degree Half-angle Cones at Mach Numbers from 0.60 to 1.30 by : Wayne J. Marko
Download or read book Static Aerodynamic Characteristics of Three Blunted Sixty-degree Half-angle Cones at Mach Numbers from 0.60 to 1.30 written by Wayne J. Marko and published by . This book was released on 1968 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Heating and Loading Within Large Open Cavities in Cone and Cone-cyclinder-flare Models at Mach 6.7 by : Lewis Roane Hunt
Download or read book Aerodynamic Heating and Loading Within Large Open Cavities in Cone and Cone-cyclinder-flare Models at Mach 6.7 written by Lewis Roane Hunt and published by . This book was released on 1974 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurement of Drag and Static Stability for a Blunt-nosed 10° Half-angle Cone at Mach Number 15 by : Dale L. Compton
Download or read book Free-flight Measurement of Drag and Static Stability for a Blunt-nosed 10° Half-angle Cone at Mach Number 15 written by Dale L. Compton and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Spherically Blunted Cones at Mach Numbers from 0.5 to 5.0 by : Robert V. Owens
Download or read book Aerodynamic Characteristics of Spherically Blunted Cones at Mach Numbers from 0.5 to 5.0 written by Robert V. Owens and published by . This book was released on 1965 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees by : Dennis M. Bushnell
Download or read book Heat-transfer and Pressure Distributions on Spherically Blunted 25 Degrees Half-angle Cone at Mach 8 and Angles of Attack Up to 90 Degrees written by Dennis M. Bushnell and published by . This book was released on 1968 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack by : Jason Paul Shimshi
Download or read book An Investigation of Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack written by Jason Paul Shimshi and published by . This book was released on 1992 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt:
