Application of Similar Solutions to Calculation of Laminar Heat Transfer on Bodies with Yaw and Large Pressure Gradient in High-speed Flow PDF Download
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Author: Ivan E. Beckwith
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 102
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Book Description
Author: Ivan E. Beckwith
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 102
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Book Description
Author: Ivan E. Beckwith
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 68
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Author:
Publisher:
ISBN:
Category : Astrophysics
Languages : en
Pages : 544
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 550
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Author:
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ISBN:
Category :
Languages : en
Pages : 520
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Outer space
Languages : en
Pages : 992
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Author: Lionel Pasiuk
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 72
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Book Description
Theoretical laminar heat transfer rates to a sphere-cone model at angles of yaw up to 18 degrees are compared with wind tunnel data measured at Mach numbers of 3.2 and 4.8. Two methods of heat transfer prediction have been chosen--the methods of Beckwith and VaglioLaurin. These require that the inviscid streamline pattern on the surface of the yawed spherecone model be known. These steamlines have been calculated from measured surface pressure distributions. The theory of Beckwith agrees reasonably well with the experimental data.
Author: D. Küchemann
Publisher: Elsevier
ISBN: 1483224880
Category : Technology & Engineering
Languages : en
Pages : 481
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Book Description
Progress in Aeronautical Sciences, Volume 9 presents the vibrational characteristics of certain aircraft. This book supplements the comprehensive account of matrix methods of structural analysis. Organized into five chapters, this volume begins with an overview of the different schemes of the numerical method of characteristics for calculating three-dimensional steady supersonic gas flow about bodies moving at incidence. This text then examines the flow of a perfect gas and provides the generalization for the case of equilibrium and non-equilibrium flow of real gas. Other chapters consider the various aspects of the aerodynamic design of aircraft and discuss the application of modern computer methods to fluid mechanics. This book discusses as well the prospects for further development of the existing types and for the establishment of the as yet hypothetical types of aircraft. The final chapter shows how the evolution of the aerodynamic shape leads to a complete spectrum of major types of aircraft. This book is a valuable resource for engineers.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 44
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