The Effect of Fluid Injection on the Compressible Turbulent Boundary Layer - The Effect on Skin Friction of Air Injected Into the Boundary Layer of a Cone at M PDF Download

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The Effect of Fluid Injection on the Compressible Turbulent Boundary Layer - The Effect on Skin Friction of Air Injected Into the Boundary Layer of a Cone at M

The Effect of Fluid Injection on the Compressible Turbulent Boundary Layer - The Effect on Skin Friction of Air Injected Into the Boundary Layer of a Cone at M PDF Author: Thorval Tendeland
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 23

Book Description


The Effect of Fluid Injection on the Compressible Turbulent Boundary Layer - The Effect on Skin Friction of Air Injected Into the Boundary Layer of a Cone at M

The Effect of Fluid Injection on the Compressible Turbulent Boundary Layer - The Effect on Skin Friction of Air Injected Into the Boundary Layer of a Cone at M PDF Author: Thorval Tendeland
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 23

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 352

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64

Book Description


Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

Book Description


WADC Technical Report

WADC Technical Report PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318

Book Description


Exploratory Investigation of Transpiration Cooling of a 40° Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures of 1,295° to 2,910° F

Exploratory Investigation of Transpiration Cooling of a 40° Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures of 1,295° to 2,910° F PDF Author: Bernard Rashis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26

Book Description
Abstract: The results presented herein were obtained in a transpiration cooling investigation of a double wedge of 40° included angle having a porous stainless-steel specimen inserted flush with the top surface of the wedge. Nitrogen and helium were used as coolants, and tests were conducted for stagnation temperatures ranging from 1,295° to 2,910° F. The data for both the nitrogen and helium coolants indicated greater cooling effectiveness than predicted by theory and were in good agreement with the results for an 8° cone tested at a stagnation temperature of 600° F.

A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

Book Description


NACA Conference on High-Speed Aerodynamics

NACA Conference on High-Speed Aerodynamics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 678

Book Description


Analytical Investigation of Reduction in Turbulent Skin Friction on a Flat Plate by Means of Air Injection Through Discrete Slots

Analytical Investigation of Reduction in Turbulent Skin Friction on a Flat Plate by Means of Air Injection Through Discrete Slots PDF Author: K. R. Czarnecki
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 70

Book Description


Progress in Aeronautical Sciences

Progress in Aeronautical Sciences PDF Author: D. Küchemann
Publisher: Elsevier
ISBN: 1483145336
Category : Technology & Engineering
Languages : en
Pages : 540

Book Description
Progress in Aeronautical Sciences, Volume 10 provides information pertinent to the development in aeronautical sciences. This book discusses a variety of topics, including thermoelasticity, turbulent boundary, as well as the manufacturing methods, reliability, problem areas, and applications under development in fluidic systems. Organized into six chapters, this volume begins with an overview of the theoretical problems of elasticity. This text then discusses the state of research in the complex fields of turbulent boundary layers with fluid injections. Other chapters consider as well the problems of supersonic flow past wings and bodies. This book discusses as well the flow in hypersonic wakes in ionized gases. The reader is also introduced to the possible applications of the compressible turbulent boundary layer with fluid injection. The final chapter discusses the components used in fluidic systems, which are described with emphasis on their general system of operation and general properties. This book is a valuable resource for engineers.