Download or read book Pressure Distribution on a Body a Revolution in Supersonic Flight written by Robert Ramon Reynolds and published by . This book was released on 1952 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution on Thin Bodies of Revolution at Supersonic Speeds written by Ernest W. Graham and published by . This book was released on with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measurements of the Drag and Pressure Distribution on a Body of Revolution Throughout Transition from Subsonic to Supersonic Speeds written by Jim Rogers Thompson and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: As part of the general investigation by the National Advisory Committee for Aeronautics of the aerodynamic characteristics of promising airplane configurations and their component parts at transonic and supersonic speeds, the drag and pressure distribution on a body of revolution of fineness ratio 12 have been measured by the free-fall method. Results are presented for Mach numbers from 0.75 to 1.27 and are the first complete measurements obtained at large scale under actual flight conditions of the pressure distribution on a body of revolution at zero angle of attack throughout the transition from subcritical to moderate supersonic speeds.
Download or read book A Pressure distribution Investigation of a Supersonic aircraft Fuselage and Calibration of the Mach Number 1 40 Nozzle of the Langley 4 by 4 foot Supersonic Tunnel written by Lowell E. Hasel and published by . This book was released on 1950 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Measurements of Pressure Distribution at Transonic and Supersonic Speeds on Bodies of Revolution Having Parabolic Afterbodies written by C. Kell and published by . This book was released on 1962 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Measurements of Pressure Distribution at Transonic and Supersonic Speeds on Bodies of Revolution Having Paralobic Afterbodies written by C. Kell and published by . This book was released on 1958 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flow Over a Slender Body of Revolution at Supersonic Velocities written by Robert T. Jones and published by . This book was released on 1946 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: The theory of small disturbances is applied to the calculation of the pressure distribution and drag of a closed body of revolution traveling at supersonic speeds. It is shown that toward the rear of the body the shape of the pressure distribution is similar to that for subsonic flow. For fineness ratios between 10 and 15 the theoretical wave drag is of the same order as probable values of the frictional drag.
Download or read book Approximate Pressure Distribution Calculations for Slender Bodies of Revolution in Axial Supersonic Flow written by Ernest W. Graham and published by . This book was released on 1948 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution on Bodies of Revolution at Supersonic Speeds written by M.H. Gheith and published by . This book was released on 1978 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Prediction Techniques for Pressure and Heat Transfer Distributions Over Bodies of Revolution in High Subsonic to Low Supersonic Flight written by L. K. Isaacson and published by . This book was released on 1968 with total page 155 pages. Available in PDF, EPUB and Kindle. Book excerpt: A literature survey and an evaluation of applicable literature concerning pressure and heat-transfer distributions over bodies of revolution in high-subsonic to low-supersonic flight are presented. Methods for determining the pressure distribution on bodies of revolution are discussed and compared with experimental data. Variations of the modified Newtonian method may be applied to a large class of bodies of revolution for free-stream Mach numbers greater than 0.75. Appropriate experimental laminar and turbulent heat-transfer data for a blunt-body vehicle at flight Mach numbers between 1.6 and 5 are compared with calculated values. Experimental data could not be found for blunt-body turbulent heat transfer in the free-stream Mach number range from 0.7 to 1.6. An extensive bibliography covering prediction techniques and experimental data on pressure and heat-transfer distributions is included as the appendix. (Author).
Download or read book Theoretical Pressure Distribution Over an Arbitrary Body of Revolution at an Angle of Attack in Supersonic Flow written by Albert Victor Spratley and published by . This book was released on 1975 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution and Some Effects of Viscosity on Slender Inclined Bodies of Revolution written by H. Julian Allen and published by . This book was released on 1950 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: The simplified solution for the pressure distribution of slender inclined bodies of revolution is developed. The solution should be suitable for bodies of high fineness ratio even at low supersonic speeds, provided the angle of attack is small. Comparison with low-speed experimental results indicates that the observed flow separation phenomena can be explained in terms of the calculated pressure distributions together with the theory of oblique viscous flows.
Download or read book The Pressure Distribution on Bodies of Revolution at Supersonic Velocities written by Vincent James Berinati and published by . This book was released on 1951 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular arc Sections and a 40 Sweepback written by John P. Gapcynski and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1950 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight written by Richard Scherrer and published by . This book was released on 1947 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was developed and applied to an example body. The cooling requirement for the example body was determined as a function of Mach number, altitude, size, and a surface-temperature parameter. The maximum value of Mach number considered was 3.0 and the altitudes considered were those within the lower constant-temperature region of the atmosphere (40,000 to 120,000 ft). The extent of the laminar boundary layer was determined approximately at each condition as a function of the variables considered.
Download or read book Handbook of Supersonic Aerodynamics written by D. Adamson and published by . This book was released on 1961 with total page 366 pages. Available in PDF, EPUB and Kindle. Book excerpt:
