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Charts For Flow Parameters Of Helium At Hypersonic Speeds Mach Number 10 To 20
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Book Synopsis Charts for Flow Parameters of Helium at Hypersonic Speeds, Mach Number 10 to 20 by : Wright Air Development Center
Download or read book Charts for Flow Parameters of Helium at Hypersonic Speeds, Mach Number 10 to 20 written by Wright Air Development Center and published by . This book was released on 1957 with total page 2 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Charts for Flow Parameters of Helium at Hypersonic Speeds by : James Forrestal Research Center. Gas Dynamics Laboratory
Download or read book Charts for Flow Parameters of Helium at Hypersonic Speeds written by James Forrestal Research Center. Gas Dynamics Laboratory and published by . This book was released on 1957 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Charts for Conical and Two-dimensional Oblique-shock Flow Parameters in Helium at Mach Numbers from about 1 to 100 by : Arthur Henderson
Download or read book Charts for Conical and Two-dimensional Oblique-shock Flow Parameters in Helium at Mach Numbers from about 1 to 100 written by Arthur Henderson and published by . This book was released on 1961 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Aspects of Air-helium Simulation and Hypersonic Approximations by : Eugene S. Love
Download or read book Some Aspects of Air-helium Simulation and Hypersonic Approximations written by Eugene S. Love and published by . This book was released on 1959 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Correlation of Oblique Shock Parameters for Ratios of Specific Heats from 1 to 5/3 with Application to Real Gas Flows by : Mitchel H. Bertram
Download or read book The Correlation of Oblique Shock Parameters for Ratios of Specific Heats from 1 to 5/3 with Application to Real Gas Flows written by Mitchel H. Bertram and published by . This book was released on 1963 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytic investigation was made to show the extent of correlation of the exact oblique shock parameters that may be accomplished by means of similarity parameters suggested by approximate theory. The exact theory for the inviscid flow of a perfect gas was calculated for Mach numbers of 1.1 to 40, ratios of specific heats from 1 to 5/3, and angles of attack from 0° to shock detachment. From consideration of the approximate theory and the concept of effective ratio of specific heats, the oblique shock correlations were found to be useful for the rapid calculation of many flow parameters for an equilibrium real gas. Some useful correlations are also given for the case of isentropic expansion around a sharp corner.
Download or read book Helium written by Carla W. Cherry and published by . This book was released on 1968 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Report written by and published by . This book was released on 1963 with total page 820 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1961 with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Review of the Hypersonic Research Carried Out at Princeton University from 1949-1955 by : Seymour M. Bogdonoff
Download or read book A Review of the Hypersonic Research Carried Out at Princeton University from 1949-1955 written by Seymour M. Bogdonoff and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Information Circular written by and published by . This book was released on 1968 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis WADC Technical Report by : United States. Wright Air Development Division
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1955 with total page 1286 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Real-gas Correction Factors for Hypersonic Flow Parameters in Helium by : Wayne Douglas Erickson
Download or read book Real-gas Correction Factors for Hypersonic Flow Parameters in Helium written by Wayne Douglas Erickson and published by . This book was released on 1960 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: The real-gas hypersonic flow parameters for helium have been calculated for stagnation temperatures from 0 F to 600 F and stagnation pressures up to 6,000 pounds per square inch absolute. The results of these calculations are presented in the form of simple correction factors which must be applied to the tabulated ideal-gas parameters. It has been shown that the deviations from the ideal-gas law which exist at high pressures may cause a corresponding significant error in the hypersonic flow parameters when calculated as an ideal gas. For example the ratio of the free-stream static to stagnation pressure as calculated from the thermodynamic properties of helium for a stagnation temperature of 80 F and pressure of 4,000 pounds per square inch absolute was found to be approximately 13 percent greater than that determined from the ideal-gas tabulation with a specific heat ratio of 5/3.
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1960 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Extension of Estimated Hypersonic Flow Parameters for Helium as a Real Gas by : Wayne Douglas Erickson
Download or read book An Extension of Estimated Hypersonic Flow Parameters for Helium as a Real Gas written by Wayne Douglas Erickson and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Real-helium Hypersonic Flow Parameters for Pressures to 3600 Atmospheres and Temperatures to 15 000° K by : Charles George Miller
Download or read book Real-helium Hypersonic Flow Parameters for Pressures to 3600 Atmospheres and Temperatures to 15 000° K written by Charles George Miller and published by . This book was released on 1968 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Real-gas Correction Factors for Hypersonic Flow Parameters in Helium by : Wayne Douglas Erickson
Download or read book Real-gas Correction Factors for Hypersonic Flow Parameters in Helium written by Wayne Douglas Erickson and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The real-gas hypersonic flow parameters for helium have been calculated for stagnation temperatures from 0 F to 600 F and stagnation pressures up to 6,000 pounds per square inch absolute. The results of these calculations are presented in the form of simple correction factors which must be applied to the tabulated ideal-gas parameters. It has been shown that the deviations from the ideal-gas law which exist at high pressures may cause a corresponding significant error in the hypersonic flow parameters when calculated as an ideal gas. For example the ratio of the free-stream static to stagnation pressure as calculated from the thermodynamic properties of helium for a stagnation temperature of 80 F and pressure of 4,000 pounds per square inch absolute was found to be approximately 13 percent greater than that determined from the ideal-gas tabulation with a specific heat ratio of 5/3.
Book Synopsis Measurement of Flow Angularity at Supersonic and Hypersonic Speeds with the Use of a Conical Probe by : Frank Edwin Swalley
Download or read book Measurement of Flow Angularity at Supersonic and Hypersonic Speeds with the Use of a Conical Probe written by Frank Edwin Swalley and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The characteristics of a 40° half-angle cone for measuring flow angularity were determined experimentally. Tests were conducted at a Mach number of 21 in helium with check points at Mach number 3.55 in air for angles of pitch up to 5°. The air tests confirmed theoretical indications of small or negligible Mach number and test-medium effects for the case of air and helium. The instrument is capable of measuring flow angularity at high Reynolds numbers and speeds greater than that necessary for shock attachment to within ± 1/3°.
