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
Author: Thorval Tendeland
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 23
Book Description
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 23
Book Description
NASA Technical Note
NASA Technical Memorandum
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
WADC Technical Report
Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
Book Description
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
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.
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 ...
NACA Conference on High-Speed Aerodynamics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 678
Book Description
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
Author: K. R. Czarnecki
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 70
Book Description
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 70
Book Description
Progress in Aeronautical Sciences
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.
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.