A Comparison of Experimental and Theoretical Results for the Compressible Turbulent-boundary-layer Skin Friction with Zero Pressure Gradient PDF Download

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A Comparison of Experimental and Theoretical Results for the Compressible Turbulent-boundary-layer Skin Friction with Zero Pressure Gradient

A Comparison of Experimental and Theoretical Results for the Compressible Turbulent-boundary-layer Skin Friction with Zero Pressure Gradient PDF Author: John B. Peterson
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 60

Book Description

A Comparison of Experimental and Theoretical Results for the Compressible Turbulent-boundary-layer Skin Friction with Zero Pressure Gradient

A Comparison of Experimental and Theoretical Results for the Compressible Turbulent-boundary-layer Skin Friction with Zero Pressure Gradient PDF Author: John B. Peterson
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
Languages : en
Pages : 60

Book Description

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF Author: David L. Brott
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 104

Book Description
The paper describes the results of a detailed experimental investigation of a two-dimensional turbulent boundary layer in a favorable pressure gradient where the free-stream Mach number varied from 3.8 to 4.6 and the ratio of wall to adiabatic-wall temperature has a nominal value of 0.82. Detailed profile measurements were made with pressure and temperature probes; skin friction was measured directly with a shear balance. The velocity- and temperature-profile results were compared with zero pressure gradient and incompressible results. The skin-friction data were correlated with momentum-thickness Reynolds number and pressure-gradient parameter. (Author).

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 434

Book Description

NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 814

Book Description

Development of a Low-aspect Ratio Fin for Flight Research Experiments

Development of a Low-aspect Ratio Fin for Flight Research Experiments PDF Author: David M. Richwine
Publisher:
ISBN:
Category : Flow visualization
Languages : en
Pages : 20

Book Description

Heat-transfer Measurements at Mach 8 on a Flat Plate with Deflected Trailing-edge Flap with Effects of Transition Included

Heat-transfer Measurements at Mach 8 on a Flat Plate with Deflected Trailing-edge Flap with Effects of Transition Included PDF Author: Charles Borden Johnson
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 60

Book Description

NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 56

Book Description

The Characteristics of a Laminar Boundary Layer on a Spinning Tangent Ogive Cylinder at Angle of Attack

The Characteristics of a Laminar Boundary Layer on a Spinning Tangent Ogive Cylinder at Angle of Attack PDF Author: H. R. Vaughn
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 56

Book Description
Streamwise velocity profiles of a laminar boundary layer were determined from pitot pressure measurements made in a supersonic wind tunnel on a spinning tangent ogive cylinder at zero and four degrees angle of attack. A transformation was found which transforms the velocity profiles to be in agreement with the incompressible Blasius profile.

New Design Concepts for High Speed Air Transport

New Design Concepts for High Speed Air Transport PDF Author: H. Sobieczky
Publisher: Springer
ISBN: 3709126584
Category : Technology & Engineering
Languages : en
Pages : 333

Book Description
This book presents the challenges, the tools and the concepts for developing economically viable high speed civil transport aircraft under environmental constraints. Computational tools for aircraft design and optimization are outlined and application in an industrial environment is shown for new and innovative case studies.

Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va

Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va PDF Author:
Publisher:
ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 528

Book Description

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