Author: Earl C. WatsonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 62
Book Description
An Experimental Investigation of the Flow in an Axisymmetric Internal-compression Inlet for M
Author: Earl C. WatsonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 62
Book Description
Scramjet Propulsion
Author: E. T. CurranPublisher: AIAA
ISBN: 9781600864414
Category : Airplanes
Languages : en
Pages : 1354
Book Description
Particle Image Velocimetry
Author: Markus RaffelPublisher: Springer Science & Business Media
ISBN: 3540723072
Category : Technology & Engineering
Languages : en
Pages : 460
Book Description
This immensely practical guide to PIV provides a condensed, yet exhaustive guide to most of the information needed for experiments employing the technique. This second edition has updated chapters on the principles and extra information on microscopic, high-speed and three component measurements as well as a description of advanced evaluation techniques. What’s more, the huge increase in the range of possible applications has been taken into account as the chapter describing these applications of the PIV technique has been expanded.
Theoretical and Experimental Investigation of Flow Over Single and Double Backward Facing Steps
Author: Douglas Eugene AbbottPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 116
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger BabinskyPublisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Scientific and Technical Aerospace Reports
Author: An Experimental Investigation of the Flow Field Around a Yawed Cone
Author: Robert H. FeldhuhnPublisher:
ISBN:
Category : Cone
Languages : en
Pages : 106
Book Description
An experimental investigation of the flow field associated with a highly yawed cone was conducted at a Mach number of 5 and a free-stream Reynolds number per foot of 4,400,000. Surface static pressure measurements, flow-field surveys and schlieren photographs were obtained on a sharp five-degree semi-vertex angle cone at an angle of attack of 24 degrees. The results of the measurements indicate that the flow field on the leeward side of a highly yawed cone is very similar to that of a circular cylinder in supersonic cross flow. The essential difference between these two flow fields is the presence of a disturbance from the tip of the cone which separates the gas which has passed through the shock wave on the windward side from the flow which has passed through the weaker portion of the shock wave on the leeward side of the cone. (Author).
An Experimental Investigation of the Surface Pitot Probe Including Effects of Heat Transfer and Compressibility
Author: David L. BrottPublisher:
ISBN:
Category : Flow meters
Languages : en
Pages : 60
Book Description
This report presents the experimental investigation of surface Pitot probe in both subsonic and supersonic flow. The effect of heat transfer on the results was also investigated in supersonic flow. (Author).
Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration
Author: Publisher:
ISBN:
Category : Outer space
Languages : en
Pages : 544
Book Description
A Chinese boy's greatest wish is to be an artist but he is too poor to buy a good brush until a wizard appears and gives him one with magic powers.
An Experimental Investigation of Transonic Flow Past Two-dimensional Wedge and Circular-arc Sections Using a Mach-Zehnder Interferometer
Author: Arthur Earl BrysonPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 106
Book Description
Interferometer measurements are given of the flow fields near two-dimensional wedge and circular-arc sections at zero angle of attack. Pressure distributions and drag coefficients as functions of Mach number were obtained and the wedge data are compared with theory. It is shown that the local Mach number at any point on the surface of a finite three dimensional body or an unswept two-dimensional body, moving through an infinite fluid, has a stationary value at Mach number 1 and, in fact, remains nearly constant for a range of speeds below and above Mach number 1. On the basis of this concept and the experimental data, pressure distributions and drag coefficients for the wedge and circular-arc sections are presented throughout the entire transonic range of velocities.