Experimental Investigation Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities
Experimental Investigation Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities

Author: Dean R. Chapman

Publisher:

Published: 1952

Total Pages: 852

ISBN-13:

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The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.

Fuel Systems for IC Engines
Fuel Systems for IC Engines

Author: Institution of Mechanical Engineers

Publisher: Elsevier

Published: 2012-03-06

Total Pages: 348

ISBN-13: 0857096044

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This book presents the papers from the latest conference in this successful series on fuel injection systems for internal combustion engines. It is vital for the automotive industry to continue to meet the demands of the modern environmental agenda. In order to excel, manufacturers must research and develop fuel systems that guarantee the best engine performance, ensuring minimal emissions and maximum profit. The papers from this unique conference focus on the latest technology for state-of-the-art system design, characterisation, measurement, and modelling, addressing all technological aspects of diesel and gasoline fuel injection systems. Topics range from fundamental fuel spray theory, component design, to effects on engine performance, fuel economy and emissions. - Presents the papers from the IMechE conference on fuel injection systems for internal combustion engines - Papers focus on the latest technology for state-of-the-art system design, characterisation, measurement and modelling; addressing all technological aspects of diesel and gasoline fuel injection systems - Topics range from fundamental fuel spray theory and component design to effects on engine performance, fuel economy and emissions

Report
Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published: 1957

Total Pages: 324

ISBN-13:

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