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Tables For Supersonic Flow Of Helium Around Right Circular Cones At Zero Angle Of Attack
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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 40 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 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:
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 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 440 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 Tables for Supersonic Flow of Helium Around Right Ciruclar Cones at Zero Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow of Helium Around Right Ciruclar Cones at Zero Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 24 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 38 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 Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack [with List of References] by :
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack [with List of References] written by and published by . This book was released on 1964 with total page 421 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones Zero Angles of Attack by : J. L. Sims
Download or read book Tables for Supersonic Flow Around Right Circular Cones Zero Angles of Attack written by J. L. Sims and published by . This book was released on 1964 with total page 421 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack by : Joseph L. Sims
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack written by Joseph L. Sims and published by . This book was released on 1964 with total page 432 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 421 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack by : Joseph Laney Sims
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack written by Joseph Laney Sims and published by . This book was released on 1964 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack [with Bibliographies] by :
Download or read book Tables for Supersonic Flow Around Right Circular Cones at Small Angle of Attack [with Bibliographies] written by and published by . This book was released on 1964 with total page 422 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 1970 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog, United States Public Documents by : United States. Superintendent of Documents
Download or read book Monthly Catalog, United States Public Documents written by United States. Superintendent of Documents and published by . This book was released on 1973 with total page 1252 pages. Available in PDF, EPUB and Kindle. Book excerpt: February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages : pages Book Rating :4.:/5 (54 download)
Book Synopsis Tables for Supersonic Flow Round Right Circular Cones at Small Angle of Attack. By Joseph L. Sims by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book Tables for Supersonic Flow Round Right Circular Cones at Small Angle of Attack. By Joseph L. Sims 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 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
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