Download or read book The Potential Theory of Unsteady Supersonic Flow written by John Wilder Miles and published by . This book was released on 1959 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Potential Theory of Unsteady Supersonic Flow written by John Wilder Miles and published by . This book was released on 1980 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady Supersonic Flow written by John Miles and published by . This book was released on 1955 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The following monograph is intended to survey they application of the theory of perfect fluid flow to the prediction of the aerodynamic forces that act on thin wings and slender bodies as a result of small, unsteady motions with respect to an equilibrium configuration of uniform, supersonic flight. In addition, certain aspects of the corresponding subsonic problem are taken up (in Chapters 1 and 2) insofar as they afford informative comparisons with their supersonic counterparts."--Preface.

Download or read book Unsteady Supersonic Flow Over a Cone with a Blunted Tip written by G. F. TELENIN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Potential Theory of Unsteady Supersonic Flow written by pseud Armiger and published by . This book was released on 1959 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady Supersonic Flow from a Tube with Continuous Energy Release written by Planjery V. Sankaranarayana and published by . This book was released on 1973 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady Aerodynamic Forces on a Slender Body of Revolution in Supersonic Flow written by Reuben Bond and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Linearized slender-body theory is applied to the computation of aerodynamic forces on an oscillating, or deforming, body in supersonic flow. The undeformed body is a body of revolution and the deformed body is represented by movement of a line through the centers of the cross sections which are assumed to remain circular. The time dependence is based on sinusoidal motion. For a body of vanishing thickness the slender-body theory yields the apparent mass approximation as it is obtained for incompressible crossflow around a cylinder. Both linearized slender-body theory and the apparent mass approximation are used to calculate the pitching-moment coefficients on a rigid slender body with a parabolic arc nose cone, and these coefficients are compared with some experimental results. (Author).

Download or read book Unsteady Supersonic Flow with Heat Addition Due to Condensation written by Francis Pierre Mosnier and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Steady and Unsteady Supersonic Flow Control with Energy Addition written by M. N. Shneider and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Second order Theory of Unsteady Supersonic Flow written by Alan King King and published by . This book was released on 1953 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady Supersonic Flow from a Tube written by C. J. Chen and published by . This book was released on 1974 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt: The strength of the shock wave in the vicinity of a gun is predicted. The energy release is considered to be a function of time. As the shock wave reaches the point of analysis the energy is still being released. It is found that the energy release by the after-flashing will not significantly alter the shock strength but will affect the flow behind the shock wave. The pressure behind the shock wave will decrease slower if the energy is released continuously. The strength of the shock wave in general decreases with increase of the length of tube and is proportional to the total energy released.

Download or read book Second Order Theory for Unsteady Super sonic Flow Past Slender Pointed Bodies of Revolution written by James Dewey Revell and published by . This book was released on 1958 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady Supersonic Combustion written by Mingbo Sun and published by Springer Nature. This book was released on 2020-04-14 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book describes the unsteady phenomena needed to understand supersonic combustion. Following an initial chapter that introduces readers to the basic concepts in and classical studies on unsteady supersonic combustion, the book highlights recent studies on unsteady phenomena, which offer insights on e.g. interactions between acoustic waves and flames, flow dominating instability, ignition instability, flame flashback, and near-blowout-limit combustion. In turn, the book discusses in detail the fundamental mechanisms of these phenomena, and puts forward practical suggestions for future scramjet design.

Download or read book Unsteady Supersonic Flow Past a Circular Cone Pitching and Plunging in a Plane written by Henry Wing H. Kan and published by . This book was released on 1980 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Unsteady Supersonic Flow by John W Miles written by University of California, Los Angeles. Department of Engineering and published by . This book was released on 1955 with total page 569 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Numerical Investigation of Unsteady Supersonic Flow in an Oscillating Cascade and a Modification to the Solid Surface Boundary Condition of an Euler Steady Flow Solver written by Edward Joseph Gallagher and published by . This book was released on 1999 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Application of a One strip Integral Method to the Unsteady Supersonic Aerodynamics of an Inclined Flat Surface written by Robert M. Bennett and published by . This book was released on 1972 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method of integral relations is applied in a one-strip approximation to the perturbation equations governing small motions of an inclined, sharp-edged, flat surface about the mean supersonic steady flow. Algebraic expressions for low reduced-frequency aerodynamics are obtained and a set of ordinary differential equations are obtained for general oscillatory motion. Results are presented for low reduced-frequency aerodynamics and for the variation of the unsteady forces with frequency. The method gives accurate results for the aerodynamic forces at low reduced frequency which are in good agreement with available experimental data. However, for cases in which the aerodynamic forces vary rapidly with frequency, the results are qualitatively correct, but of limited accuracy. Calculations indicate that for a range of inclination angles near shock detachment such that the flow in the shock layer is low supersonic, the aerodynamic forces vary rapidly both with inclination angle and with reduced frequency.