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Correlation Graphs For Supersonic Flow Around Right Circular Cones At Zero Yaw In Air As A Perfect Gas
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Book Synopsis Correlation Graphs for Supersonic Flow Around Right Circular Cones at Zero Yaw in Air as a Perfect Gas by : Mitchel H. Bertram
Download or read book Correlation Graphs for Supersonic Flow Around Right Circular Cones at Zero Yaw in Air as a Perfect Gas written by Mitchel H. Bertram and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concise accurate graphs of cone flow properties at zero yaw in air as a perfect gas are presented in correlation form. From these graphs the pressure, density, temperature, shock angle, and Mach number may be obtained both at the cone surface and immediately behind the shock, for free-stream Mach numbers from that for shock detachment to that approaching infinity and for cone semi -apex angles up to 50°. In addition, the initial slope of the normal-force curve is given for the same range of conditions.
Book Synopsis Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium. Part Ii. Tables of Data by : Henry E Hudgins (Jr)
Download or read book Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium. Part Ii. Tables of Data written by Henry E Hudgins (Jr) and published by . This book was released on 1964 with total page 825 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part I (AD-468 284) of this report is an analysis of the inviscid flow fields for air in chemical equilibrium about right circular cones at zero yaw. Parts II and III present, in tabular form, the results of the calculation of real gas supersonic flow fields about right circular cones at zero angle of yaw upon which the correlation analysis in Part I is based. The calculations were performed by a numerical integration of the conical flow equations written in terms of a single geometric parameter, the ray angle eta; thus, the results are independent of body size. Flow properties are given along rays which are defined by 10 equal angular increments between the shock and cone surface. Numerical calculations were performed utilizing the Picatinny Arsenal IBM 709/90/94 Conical Flow Field Program. Results are obtained for cone semi-angles from 2.5 degrees to 50 degrees, altitudes from 0 to 200,000 ft, and Mach numbers from 3 to 40, excluding those which result in a detached shock or are well within the ideal gas regime. (Author).
Download or read book NASA Technical Note written by and published by . This book was released on 1968 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1973 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.
Book Synopsis Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium, Part Iii. Tables of Data, Cont by : Henry E Hudgins (Jr)
Download or read book Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium, Part Iii. Tables of Data, Cont written by Henry E Hudgins (Jr) and published by . This book was released on 1964 with total page 817 pages. Available in PDF, EPUB and Kindle. Book excerpt: This material is a continuation of Part II and presents the cone flow properties of air in chemical equilibrium for altitudes from 100,000 to 200,000 feet at cone angles of 2.5 to 50 degrees, and various Mach numbers from 3.0 to 40.0. Part II presents the cone properties for altitudes from sea level to 80,000 feet. Part I presents an analysis and correlation of this data. The Table of Symbols has been reproduced in this report for the convenience of the reader. (Author).
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 462 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :1156 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1964 with total page 1156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1979 with total page 1250 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Flow Around Right Circular Cones, Tables for Zero Angle of Attack by : Joseph L. Sims
Download or read book Supersonic Flow Around Right Circular Cones, Tables for Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1960 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 ̊in Helium by : Dal V. Maddalon
Download or read book Aerodynamic Characteristics of the Sharp Right Circular Cone at Mach 20.3 and Angles of Attack to 110 ̊in Helium written by Dal V. Maddalon and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20 by : Theodore R. Creel
Download or read book Pressure Distributions and Aerodynamic Characteristics of 90 and 150 Blunted Cones in Nitrogen and Helium at Mach 20 written by Theodore R. Creel and published by . This book was released on 1968 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft, Volume 1 by :
Download or read book Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft, Volume 1 written by and published by . This book was released on 1980 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Drag of Slightly Blunted Slender Cones by : W. Carson Lyons (Jr.)
Download or read book The Drag of Slightly Blunted Slender Cones written by W. Carson Lyons (Jr.) and published by . This book was released on 1968 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program is presented for calculating the various components comprising the total drag coefficient for slightly blunted slender cones. The program is applicable for either the case of a completely laminar boundary layer or where transition occurs on the cone. Weak viscous interaction effects are taken into account. Local flow properties which exist at the outer edge of the boundary layer along the cone are also computed. (Author).
Book Synopsis Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft by : Mark R. Nichols
Download or read book Bibliography on Aerodynamics of Airframe/engine Integration of High-speed Turbine-powered Aircraft written by Mark R. Nichols and published by . This book was released on 1980 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1958 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 1964 with total page 1592 pages. Available in PDF, EPUB and Kindle. Book excerpt:
