Author: Youngbin YoonPublisher:
ISBN:
Category :
Languages : en
Pages : 316
Book Description
An Experimental Study of a Generic Supersonic Combustor
Author: Youngbin YoonPublisher:
ISBN:
Category :
Languages : en
Pages : 316
Book Description
An Experimental Study of Supersonic Hydrogen-air Flames for Scramjet Applications
Author: Hwanil HuhPublisher:
ISBN:
Category :
Languages : en
Pages : 340
Book Description
A Numerical and Experimental Study of a Supersonic Combustor Employing Swept Ramp Fuel Injectors
Author: Dean R. EklundPublisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Design and Experimental Study of Injection Systems in a Supersonic Combustion Chamber
Author: Sara Rocci DenisPublisher:
ISBN:
Category :
Languages : en
Pages : 153
Book Description
Analytical and Experimental Study of Supersonic Combustion of Hydrogen in a Vitiated Airstream
Author: Marshall C. BurrowsPublisher:
ISBN:
Category :
Languages : en
Pages : 25
Book Description
Experimental Study of Cavity-strut Combustion in Supersonic Flow (postprint)
Author: K.-Y. HsüPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 14
Book Description
An experimental investigation of cavity-based flameholders with strut injectors in a supersonic flow is reported. In this ongoing research program, emphases are placed on understanding cavity-based flameholders and providing alternative methods for improving overall combustor performance in scramjet engines. Three different struts with fuel injectors are mounted near the cavity leading edge to study flame propagation and ignition of fuel in the core flow region. OH-PLIF (planar laser induced fluorescence) is used to identify the flame zone around the cavity and strut-wake regions over a range of conditions. Shadowgraphy is used to capture the flow features around the strut and cavity. In-stream probing is conducted to characterize the flow features associated with the different strut configurations. Stagnationtemperature profiles are obtained for all struts operating over the same conditions in the combusting-flow study. Two cavity fueling schemes are used to compare flameholder performance. Direct cavity air injection is found to improve combustion significantly. For each strut, upstream and downstream fueling schemes are compared over a range of conditions.--P. i.
Experimental Study of Compressibility Effects on Entrainment and Mixing in Supersonic Planar Turbulent Bluff-body Wakes
Author: Masaki NakagawaPublisher:
ISBN:
Category :
Languages : en
Pages : 448
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Turbulent Reacting Flows and Supersonic Combustion
Author: C. T. BowmanPublisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
An experimental and computational investigation of supersonic combustion flows was carried out. The principal objective of the research was to gain a more fundamental understanding of mixing and chemical reaction in supersonic flows. The research effort comprised three inter-related elements: (1) an experimental study of mixing and combustion in a supersonic plane mixing layer; (2) development of laser-induced fluorescence techniques for time-resolved two-dimensional imaging of species concentration, temperature and velocity; and (3) numerical simulations of compressible reacting flows. The specific objectives and the results of the research is summarized. Keywords: Turbulent reacting flow; Supersonic combustion. (jhd).
Experimental Study of Supersonic Flow in the Prandtl Nozzle
Author: J. W. DolanPublisher:
ISBN:
Category :
Languages : en
Pages : 68
Book Description
