Author: Benjamin J. Day
Publisher:
ISBN:
Category :
Languages : en
Pages : 103
Book Description
Turbulence Measurements in Supersonic Jets with Optical Deflectometry
Turbulence Measurements in Supersonic, Shock-free Jets by the Optical Crossed-beam Method
Investigation with an Interferometer of the Turbulent Mixing of a Free Supersonic Jet
Author: Paul B. Gooderum
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 74
Book Description
The free turbulent mixing of a supersonic jet was investigated with an interferometer, of which a description is given. Density and velocity distributions through the mixing zone were obtained. The velocity distribution was found to be similar to those for imcompressible jets over only the subsonic portion of the mixing pattern.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 74
Book Description
The free turbulent mixing of a supersonic jet was investigated with an interferometer, of which a description is given. Density and velocity distributions through the mixing zone were obtained. The velocity distribution was found to be similar to those for imcompressible jets over only the subsonic portion of the mixing pattern.
Optical Probing of Supersonic Aerodynamic Turbulence with Statistical Correlation
Author: B. H. Funk
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 148
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 148
Book Description
The Generation and Radiation of Supersonic Jet Noise: Jet flow measurement and analysis with special emphasis on remote sensing devices
Author: Lockheed-Georgia Company
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 322
Book Description
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 322
Book Description
Meanflow and Turbulence Measurements in the Wake of a Supersonic Through-flow Cascade
Author: Rodney Dale Welch Bowersox
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 392
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 392
Book Description
Turbulence Measurements in Supersonic Flow with the Hot-wire Anemometer
Study of Turbulent Supersonic Flow Based on the Optical and Acoustic Measurements
Author: Viktor Banakh
Publisher:
ISBN:
Category : Science
Languages : en
Pages :
Book Description
Study of Turbulent Supersonic Flow Based on the Optical and Acoustic Measurements.
Publisher:
ISBN:
Category : Science
Languages : en
Pages :
Book Description
Study of Turbulent Supersonic Flow Based on the Optical and Acoustic Measurements.
Some Optical Techniques for Temperature and Concentration Measurements of Combustion in Supersonic Streams
Author: Erwin A. Lezberg
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 32
Book Description
Turbulent Shear Layers in Supersonic Flow
Author: Alexander J. Smits
Publisher: Springer Science & Business Media
ISBN: 0387263055
Category : Science
Languages : en
Pages : 418
Book Description
A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.
Publisher: Springer Science & Business Media
ISBN: 0387263055
Category : Science
Languages : en
Pages : 418
Book Description
A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.