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Author: MARC BROWN Publisher: ISBN: 9780001714540 Category : Readers Languages : en Pages : 28
Book Description
"Wings! Wings! Wings! They are wonderful flying things . . ". Come join Marc Brown for a wacky, whimsical whirl through the world of winged things. Kids will learn about creatures and things that have wings. Brown's dazzling, bold art perfectly complements his easy-to-read rhyming text. Full color.
Author: MARC BROWN Publisher: ISBN: 9780001714540 Category : Readers Languages : en Pages : 28
Book Description
"Wings! Wings! Wings! They are wonderful flying things . . ". Come join Marc Brown for a wacky, whimsical whirl through the world of winged things. Kids will learn about creatures and things that have wings. Brown's dazzling, bold art perfectly complements his easy-to-read rhyming text. Full color.
Author: Sidney M. Harmon Publisher: ISBN: Category : Aerofoils Languages : en Pages : 42
Book Description
The method of relating the solution of a flow field to the solution of a simpler or known boundary-value problem is extended, subject to edge corrections for finite plan forms, to the most general type of prescribed boundary conditions on a wing in the linearized potential field at subsonic and supersonic speeds. The general procedure for determining edge corrections is given specific "correspondence formulas" are developed for rectangular wings at subsonic and supersonic speeds for cases that do not require the solution of an integral equation.
Author: Alberta Y. Alksne Publisher: ISBN: Category : Aerodynamics, Transonic Languages : en Pages : 58
Book Description
A method employed heretofore by the authors to obtain approximate solutions of the transonic flow equation for plane and axisymmetric flow is extended to give reasonable results for wings of finite span, consistent with the known properties of transonic flows. In this method the partial differential equation appropriate to the study of transonic flow is replaced by a nonlinear ordinary differential equation which can be solved by numerical methods. Asymptotic forms of this differential equation are given for very high and very low aspect ratios and analytic results are obtained for certain special cases. Numerical results, calculated by use of electronic computing machines, are given in the form of pressure distribution and pressure drag for two profile shapes, wedge and circular arc, for wings of rectangular plan form. The range of aspect ratios covered extends effectively from zero to infinity and agreement with the asymptotic results is shown at both limits.
Author: MARC BROWN
Author: MARC BROWN
Author: Sidney M. Harmon
Author: 
Author: 
Author: Alberta Y. Alksne
Author: United States. National Advisory Committee for Aeronautics
Author: United States. Army Air Forces
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics