Index Catalog // ScholarsArchive@OSU

An exact method of determining the spreading of a supersonic jet exhausting into a supersonic free stream

Creator:: Tschang, Pin-seng
Resource Type:: Masters Thesis
Full Text:: - .......:"-'"'-"'-"'. . - - - - - \i-.:lb&a ot ..,.,..~-ol i.o~oal ..,.UMHIJ"Us .,..._ _________ _ ,. -.,;-llior

Performance and optimum design analysis/ computation for propeller type wind turbines

Creator:: Walker, Stel Nathan
Abstract:: Development of a performance analysis for propeller type wind turbines is presented. The analysis uses a strip theory approach that includes tip-loss and blade interference. A comparison is presented between analysis and test data. The comparison indicates that the analysis predicts wind turbine performance to an accuracy that is within...
Resource Type:: Dissertation
Full Text:: many. It is with pleasure that I acknowledge their assistance. Dr. Robert F. Wilson, my major

Calculation of the pressure distribution on a pitching airfoil with application to the Darrieus Rotor

Creator:: Ghodoosian, Nader
Abstract:: An analytical model leading to the pressure distribution on the cross section of a Darrieus Rotor Blade (airfoil) was constructed. The model was based on the inviscid flow theory and the contribution of the nonsteady wake vortices was neglected. The analytical model was translated into a computer code in order...
Resource Type:: Masters Thesis
Full Text:: Abstract approved: Robert E. Wilson An analytical model leading to the pressure distribution on

An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles

Creator:: Schmitz, Bruce Wayne
Resource Type:: Masters Thesis
Full Text:: Mr. Robert E. Wilson for his advise and assistance throughout the writing o this paper. TtBLE

Effect of initial conditions on the convergence rate of the energy equation in Couette flow

Creator:: Seddigh, Foad
Abstract:: Computers are very efficient in handling the problems which deal with iteration. Numerical treatment of the unsteady energy equation is one sort of iteration. The convergence of the unsteady film coefficient, in two dimensional space, to its steady state value has been deduced by comparison of the results of the...
Resource Type:: Masters Thesis
Full Text:: Redacted for privacy Abstract approved (Associate Professor R. E. Wilson) Computers are very efficient

An application of the Newtonian boundary condition to supersonic jets exhausting into a hypersonic stream

Creator:: Newton, John Francis
Resource Type:: Masters Thesis
Full Text:: to express his appreciation for the advice and assistance received from Mr. ;obert E. Wilson of the

The effect of a canard surface on the total lift of an unswept wing in subsonic flow

Creator:: Rasmussen, Maurice Lee
Resource Type:: Masters Thesis
Full Text:: ..... .. . .... ........... . . 1 . .... i Solnenclature

The design and construction of a small intermittent supersonic wind tunnel

Creator:: Bithell, Robin Allan
Resource Type:: Masters Thesis
Full Text:: wishes to express his thanks to 1r. Robert . Wilson of the echanical Enineerinp Department whose aid

Linearized model for wind turbines in yaw

Creator:: Chaiyapinunt, Somsak
Abstract:: The analysis of rigid hub, three-bladed horizontal-axis, axisymmetric wind turbines in yaw is made using a linearized, four-degree-of-freedom model. The linearized equations of motion of rotor and nacelle are developed using quasi-steady blade element theory and Lagrange's equations. The yaw behavior of the system is studied from coefficients of the...
Resource Type:: Dissertation
Full Text:: ACKNOWLEGMENTS I would like to express my sincere gratitude to Dr. Robert E. Wilson, my major professor, for

Turbulence induced loads on a teetered rotor

Creator:: Weber, Timothy L.
Abstract:: Development of variable speed horizontal axis wind turbines has resulted in a need for an analysis code with a rotor speed degree-of-freedom. This study develops a five degree-of-freedom time domain computer code that evaluates blade and rotor, mean and cyclic loads with nonlinear aerodynamics together with atmospheric turbulence as a...
Resource Type:: Dissertation
Full Text:: Abstract approved: Robert E. Wilson Development of variable speed horizontal axis wind turbines has

ScholarsArchive@OSU

An exact method of determining the spreading of a supersonic jet exhausting into a supersonic free stream

Performance and optimum design analysis/ computation for propeller type wind turbines

Calculation of the pressure distribution on a pitching airfoil with application to the Darrieus Rotor

An analytical study of the effect of characteristic engine performance parameters on the payload capabilities of various high performance missiles

Effect of initial conditions on the convergence rate of the energy equation in Couette flow

An application of the Newtonian boundary condition to supersonic jets exhausting into a hypersonic stream

The effect of a canard surface on the total lift of an unswept wing in subsonic flow

The design and construction of a small intermittent supersonic wind tunnel

Linearized model for wind turbines in yaw

Turbulence induced loads on a teetered rotor

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