An experimental study of fluctuating wall pressures in a highly swept, sharp fin-induced, Mach 5 shock wave/turbulent boundary layer interaction

An experimental study of fluctuating wall pressures in a highly swept, sharp fin-induced, Mach 5 shock wave/turbulent boundary layer interaction PDF Author: John David Schmisseur
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 382

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An experimental study of fluctuating wall pressures in a highly swept, sharp fin-induced, Mach 5 shock wave/turbulent boundary layer interaction

An experimental study of fluctuating wall pressures in a highly swept, sharp fin-induced, Mach 5 shock wave/turbulent boundary layer interaction PDF Author: John David Schmisseur
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 382

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An Experimental Study of Fluctuating Wall Pressures in a Highly Swept, Sharp Fin-Induced, Mach 5 Shock Wave/Turbulent

An Experimental Study of Fluctuating Wall Pressures in a Highly Swept, Sharp Fin-Induced, Mach 5 Shock Wave/Turbulent PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 150

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Fluctuating wall pressure measurements have been made beneath the shock wave/turbulent boundary layer interaction generated by a sharp, unswept fin at angle of attack. Tests were conducted at Mach 5 with a freestream unit Reynolds number of 47.88 x 106 /m. The boundary layer developed naturally on the tunnel floor under approximately adiabatic temperature conditions. From visual inspection and standard time series analysis of fluctuating wall pressure signals, it has been shown that the separation shock wave undergoes a translating, intermittent type motion for fin angles between 16 and 28 degrees. Both the mean wall pressures and higher order moments are quasi-conically symmetric when collapsed in a conical coordinate system. Finally, the maximum wall pressure standard deviation in the intermittent region has been shown to scale with the sweep of the interaction and not with the inviscid pressure rise as has been previously suggested in the literature ... Shock wave, Boundary layer, Turbulent interaction, Interaction unsteadiness.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 836

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Masters Theses in the Pure and Applied Sciences

Masters Theses in the Pure and Applied Sciences PDF Author: Wade H. Shafer
Publisher: Springer Science & Business Media
ISBN: 1461524539
Category : Science
Languages : en
Pages : 391

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Masters Theses in the Pure and Applied Sciences was first conceived, published, and disseminated by the Center for Information and Numerical Data Analysis and Synthesis (CINDAS)* at Purdue University in 1957, starting its coverage of theses with the academic year 1955. Beginning with Volume 13, the printing and dis semination phases of the activity were transferred to University Microfilms/Xerox of Ann Arbor, Michigan, with the though that such an arrangement would be more beneficial to the academic and general scientific and technical community. After five years of this joint undertaking we had concluded that it was in the interest of all concerned if the printing and distribution of the volumes were handled by an international publishing house to assure improved service and broader dissemi nation. Hence, starting with Volume 18, Masters Theses in the Pure and Applied Sciences has been disseminated on a worldwide basis by Plenum Publishing Corporation of New York, and in the same year the coverage was broadened to include Canadian universities. All back issues can also be ordered from Plenum. We have reported in Volume 37 (thesis year 1992) a total of 12,549 thesis titles from 25 Canadian and 153 United States universities. We are sure that this broader base for these titles reported will greatly enhance the value of this impor tant annual reference work. While Volume 37 reports theses submitted in 1992, on occasion, certain uni versities do report theses submitted in previous years but not reported at the time.

Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 726

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
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Category : Mechanics, Applied
Languages : en
Pages : 348

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An experimental study of wall pressure fluctuations near separation in a Mach 5, sharp fin-induced turbulent interaction

An experimental study of wall pressure fluctuations near separation in a Mach 5, sharp fin-induced turbulent interaction PDF Author: Berry Thomas Gibson
Publisher:
ISBN:
Category : Wall pressure (Aerodynamics)
Languages : en
Pages : 300

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AIAA 27th Aerospace Sciences Meeting

AIAA 27th Aerospace Sciences Meeting PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 476

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Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312)

Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 392

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NASA SP.

NASA SP. PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 654

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