The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method

Download The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method by : Donald Charles Baxter

Download or read book The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method written by Donald Charles Baxter and published by . This book was released on 1957 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Similar Solutions for the Compressible Boundary Layer on a Yawed Cylinder with Transpiration Cooling

Download Similar Solutions for the Compressible Boundary Layer on a Yawed Cylinder with Transpiration Cooling PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis Similar Solutions for the Compressible Boundary Layer on a Yawed Cylinder with Transpiration Cooling by : Ivan E. Beckwith

Download or read book Similar Solutions for the Compressible Boundary Layer on a Yawed Cylinder with Transpiration Cooling written by Ivan E. Beckwith and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer and skin-friction parameters obtained from exact solutions to the laminar compressible boundary-layer equations for infinite cylinders in yaw are presented. The effects of transpiration cooling, Prandtl number, pressure gradient, wall temperature, and viscosity relation were investigated. It is shown that as the Mach number is increased for a given large yaw angle the effects of pressure gradient become larger and the quantity of coolant required to maintain a given wall temperature is also increased. The use of a linear viscosity-temperature relation gives approximately the same results as the Sutherland viscosity-temperature relation except for very high aerodynamic heating rates.

Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control

Download Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 348 pages
Book Rating : 4.3/5 (243 download)

DOWNLOAD NOW!


Book Synopsis Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control by : Benjamin Milwitzky

Download or read book Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control written by Benjamin Milwitzky and published by . This book was released on 1955 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Analysis of Once-per-revolution Oscillating Aerodynamic Thrust Loads on Single-rotation Propellers on Tractor Airplanes at Zero Yaw

Download An Analysis of Once-per-revolution Oscillating Aerodynamic Thrust Loads on Single-rotation Propellers on Tractor Airplanes at Zero Yaw PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 160 pages
Book Rating : 4.3/5 (243 download)

DOWNLOAD NOW!


Book Synopsis An Analysis of Once-per-revolution Oscillating Aerodynamic Thrust Loads on Single-rotation Propellers on Tractor Airplanes at Zero Yaw by : Franklin K. Moore

Download or read book An Analysis of Once-per-revolution Oscillating Aerodynamic Thrust Loads on Single-rotation Propellers on Tractor Airplanes at Zero Yaw written by Franklin K. Moore and published by . This book was released on 1956 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note

Download Technical Note PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 440 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Technical Note by :

Download or read book Technical Note written by and published by . This book was released on 1954 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note - National Advisory Committee for Aeronautics

Download Technical Note - National Advisory Committee for Aeronautics PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 460 pages
Book Rating : 4.3/5 (243 download)

DOWNLOAD NOW!


Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

Download Report PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Report by : United States. National Advisory Committee for Aeronautics

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Tensile and Compressive Stress-strain Properties of Some High-strength Sheet Alloys at Elevated Temperatures

Download Tensile and Compressive Stress-strain Properties of Some High-strength Sheet Alloys at Elevated Temperatures PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 672 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Tensile and Compressive Stress-strain Properties of Some High-strength Sheet Alloys at Elevated Temperatures by : Philip J. Hughes

Download or read book Tensile and Compressive Stress-strain Properties of Some High-strength Sheet Alloys at Elevated Temperatures written by Philip J. Hughes and published by . This book was released on 1954 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Representative tensile and compressive stress-strain curves are give for each material at the test temperatures. The variations of the tensile and compressive properties with temperature is shown for specimens tested parallel and transverse to the rolling direction of the materials. Secant and tangent moduli, obtained from the compressive data, are included.

Simple Methods for Classification and Construction of Similarity Solutions of Partial Differential Equations

Download Simple Methods for Classification and Construction of Similarity Solutions of Partial Differential Equations PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Simple Methods for Classification and Construction of Similarity Solutions of Partial Differential Equations by : Douglas Eugene Abbott

Download or read book Simple Methods for Classification and Construction of Similarity Solutions of Partial Differential Equations written by Douglas Eugene Abbott and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stagnation-point Flow of a Variable-property Fluid at Low Reynolds Numbers

Download Stagnation-point Flow of a Variable-property Fluid at Low Reynolds Numbers PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 360 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Stagnation-point Flow of a Variable-property Fluid at Low Reynolds Numbers by : Michael Lenard

Download or read book Stagnation-point Flow of a Variable-property Fluid at Low Reynolds Numbers written by Michael Lenard and published by . This book was released on 1962 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt: Steady, viscous, two-dimensional and axially symmetric stagnation-point flows of a gas are considered for the case when the Reynolds number is too low for the applicability of the classical boundary-layer theory. It is assumed that the low-density gas is still a continuous fluid, permitting the use of the Navier-Stokes and as associated equations as the basis of the problem. The effects of low Reynolds number are determined by applying an expansion procedure to the fluid dynamical equations.

Advances in Heat Transfer

Download Advances in Heat Transfer PDF Online Free

Author :
Publisher : Academic Press
ISBN 13 : 0080575587
Total Pages : 471 pages
Book Rating : 4.0/5 (85 download)

DOWNLOAD NOW!


Book Synopsis Advances in Heat Transfer by :

Download or read book Advances in Heat Transfer written by and published by Academic Press. This book was released on 1967-01-01 with total page 471 pages. Available in PDF, EPUB and Kindle. Book excerpt: Advances in Heat Transfer

Applied Mechanics Reviews

Download Applied Mechanics Reviews PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 776 pages
Book Rating : 4.:/5 (26 download)

DOWNLOAD NOW!


Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1971 with total page 776 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Boundary Layer and Flow Control

Download Boundary Layer and Flow Control PDF Online Free

Author :
Publisher : Elsevier
ISBN 13 : 1483226662
Total Pages : 768 pages
Book Rating : 4.4/5 (832 download)

DOWNLOAD NOW!


Book Synopsis Boundary Layer and Flow Control by : G. V. Lachmann

Download or read book Boundary Layer and Flow Control written by G. V. Lachmann and published by Elsevier. This book was released on 2014-05-12 with total page 768 pages. Available in PDF, EPUB and Kindle. Book excerpt: Boundary Layer and Flow Control: Its Principles and Application, Volume 2 focuses on the layer of fluid in the immediate area of a bounding surface where the effects of viscosity are substantial. This book is organized into two main topics—boundary layer control for low drag, and shock-induced separation and its prevention by design and boundary layer control. It specifically discusses the nature of transition, effect of two-dimensional and isolated roughness on laminar flow, and progress in the design of low drag aerofoils. The onset of separation effects for aerofoils and wings, shock-induced separation for laminar boundary layers, and shock-induced separation for laminar boundary layers are also deliberated. This volume is recommended to physicists and specialists interested in boundary layer and flow control.

Report

Download Report PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 1138 pages
Book Rating : 4.:/5 (319 download)

DOWNLOAD NOW!


Book Synopsis Report by :

Download or read book Report written by and published by . This book was released on 1958 with total page 1138 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Report - Jet Propulsion Laboratory, California Institute of Technology

Download Technical Report - Jet Propulsion Laboratory, California Institute of Technology PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Technical Report - Jet Propulsion Laboratory, California Institute of Technology by : Jet Propulsion Laboratory (U.S.)

Download or read book Technical Report - Jet Propulsion Laboratory, California Institute of Technology written by Jet Propulsion Laboratory (U.S.) and published by . This book was released on 1965 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Annual Report - National Advisory Committee for Aeronautics

Download Annual Report - National Advisory Committee for Aeronautics PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations

Download An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 608 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations by : Harry Press

Download or read book An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations written by Harry Press and published by . This book was released on 1958 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis of available airplane measurements of vertical gust velocity is presented in order to arrive at a simple description of the frequency and intensity of gust velocities experienced by airplanes in operations. For the purpose of application to missile operations; the results obtained are modified to eliminate the effects of storm-avoidance procedures normally followed in airplane operations. The frequency distributions of gust velocity are then converted to a form appropriate for use in power spectral response calculations. Methods of applying the results to the estimation of the large and the small repeated loads in missile operations are then developed. Simple methods of estimating the gust loadings that will be exceeded with a given probability are presented in terms of missile response parameters and turbulence parameters. The limitations of the present results are also discussed briefly.