Nonlinear Conical Flow
Author | : Boris Mikhaĭlovich Bulakh |
Publisher | : |
Total Pages | : 346 |
Release | : 1985 |
Genre | : Mathematics |
ISBN | : |
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Author | : Boris Mikhaĭlovich Bulakh |
Publisher | : |
Total Pages | : 346 |
Release | : 1985 |
Genre | : Mathematics |
ISBN | : |
Author | : E. B. Klunker |
Publisher | : |
Total Pages | : 92 |
Release | : 1971 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
A computational technique, called the method of lines, is developed for computing the flow field about conical configurations at incidence in a supersonic flow. The method, which makes use of the self-similarity property, is developed for the nonlinear flow equations. The method has proved to be an efficient and versatile procedure for constructing the numerical solutions to conical flow problems. It has been successful in computing the flow about circular and elliptic cones at conditions where small regions of supersonic cross flow develop and for the conical delta wings where the region of supersonic cross flow is extensive. The calculations made for circular and elliptic cones as well as for the compression side of various conical delta wings are in good agreement with experiment except in regions where viscous effects become important.
Author | : E. B. Klunker |
Publisher | : |
Total Pages | : 92 |
Release | : 1971 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
A computational technique, called the method of lines, is developed for computing the flow field about conical configurations at incidence in a supersonic flow. The method, which makes use of the self-similarity property, is developed for the nonlinear flow equations. The method has proved to be an efficient and versatile procedure for constructing the numerical solutions to conical flow problems. It has been successful in computing the flow about circular and elliptic cones at conditions where small regions of supersonic cross flow develop and for the conical delta wings where the region of supersonic cross flow is extensive. The calculations made for circular and elliptic cones as well as for the compression side of various conical delta wings are in good agreement with experiment except in regions where viscous effects become important.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 714 |
Release | : 1948 |
Genre | : Aeronautics |
ISBN | : |
Author | : C. W. Chiang |
Publisher | : |
Total Pages | : 44 |
Release | : 1970 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Author | : Dajun Guo |
Publisher | : Academic Press |
Total Pages | : 286 |
Release | : 2014-05-10 |
Genre | : Mathematics |
ISBN | : 1483261905 |
Notes and Reports in Mathematics in Science and Engineering, Volume 5: Nonlinear Problems in Abstract Cones presents the investigation of nonlinear problems in abstract cones. This book uses the theory of cones coupled with the fixed point index to investigate positive fixed points of various classes of nonlinear operators. Organized into four chapters, this volume begins with an overview of the fundamental properties of cones coupled with the fixed point index. This text then employs the fixed point theory developed to discuss positive solutions of nonlinear integral equations. Other chapters consider several examples from integral and differential equations to illustrate the abstract results. This book discusses as well the fixed points of increasing and decreasing operators. The final chapter deals with the development of the theory of nonlinear differential equations in cones. This book is a valuable resource for graduate students in mathematics. Mathematicians and researchers will also find this book useful.
Author | : A.I. Leonov |
Publisher | : Springer Science & Business Media |
Total Pages | : 492 |
Release | : 2012-12-06 |
Genre | : Technology & Engineering |
ISBN | : 9401112584 |
This monograph presents theoretical and experimental studies of flows of elastic liquids. Falling into this category are particularly the melts and concentrated solutions of such flexible-chain polymers as polyethylene, polyisobutylene and polypropylene, all of which are widely used in polymer processing. These polydisperse polymers vary greatly, from batch to batch, in their mechanical properties and 20% variation in a property is believed to be good enough. l 7 All recent books - devoted to the rheology of polymers do not answer the question of which constitutive equations should be used for solving the fluid mechanic problems of polymer processing in the usual case of an appreciable nonlinear region of deformation where nonlinear effects of shear and extensional elasticity are very important. Viscoelastic constitut ive equations cited commonly (see, e.g. Refs 5 and 6) do not describe simultaneously even the simplest cases of deformations, viz. simple shear and uniaxial extension. Moreover, some of them are internally inconsist ent and sometimes display highly unstable behaviour in simple flows without any fundamental reasons. Even more respected molecular ap free from these defects.
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 950 |
Release | : 1971 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Arnaud Couairon |
Publisher | : |
Total Pages | : 149 |
Release | : 2007 |
Genre | : Science |
ISBN | : 9788854812086 |