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Repeated stress tests on carbon steels variously heat treated

Creator:: Morris, Homer Blair
Resource Type:: Masters Thesis
Full Text:: 0.188" ,]." sauge length. Note; }ead1ngs are for an Average of two tests. No. 1 Ultimate Load

The significance and measurement of the Tsai-Wu normal interaction parameter F₁₂

Creator:: Hansen, William Christian
Resource Type:: Masters Thesis
Full Text:: (note the exaggerated scale on the 02 axis), or strain space Figure 6, the effect of differing values

Practical application of steady-state 6-DoF aerodynamic model for vehicle system loads analysis

Creator:: Torris, Connor J.
Abstract:: This work develops the Global Formula Racing computational fluid dynamics (CFD) model in StarCCM+ to allow for vehicle attitude studies to be ran to evaluate Formula Student (FS) vehicle aerodynamic loads. Attitudes that this model allows to be studied include roll, pitch, yaw, heave, tire angle, and vehicle speed. The...
Resource Type:: Masters Thesis
Full Text:: . Title: PRACTICAL APPLICATION OF STEADY-STATE 6-DOF AERODYNAMIC MODEL FOR VEHICLE SYSTEM LOADS ANALYSIS

Design and construction of an improved conductor vibration recorder

Creator:: Moore, Edward Harry
Resource Type:: Masters Thesis
Full Text:: vibration dampers of the type developed by R. F. Steidel, and shown in Appendix Drawing No. M-l-2, were

Dynamic modeling, control and linear theory of a projectile equipped with a rotating internal part

Creator:: Frost, Geoffrey W.
Abstract:: Dynamic modeling of the atmospheric flight mechanics of a projectile equipped with an uncontrolled internal rotating disk is investigated and a modified projectile linear theory is established. It is shown through modeling of this type of projectile that several coefficients of the epicyclic dynamics are altered, leading to changes in...
Resource Type:: Dissertation
Full Text:: ............................................................ 5 NOMENCLATURE ................................................... 6 INTRODUCTION

Model predictive control of a direct fire projectile equipped with canards

Creator:: Ollerenshaw, Douglas R.
Abstract:: Launch uncertainties in uncontrolled direct fire projectiles can lead to significant impact point dispersion, even at relatively short range. A model predictive control scheme for direct fire projectiles is investigated to reduce impact point dispersion. The control law depends on projectile linear theory to create an approximate linear model of...
Resource Type:: Masters Thesis
Full Text:: ," Journal ofGuidance, Control, and Dynamics, Vol. 6, No. 4, pp. 280-286, 1983. 12. Cobb K.K., Whyte RH

An investigation of domestic oil heating with special emphasis on warm-air furnaces

Creator:: Kollas, Wilhelm James
Resource Type:: Masters Thesis
Full Text:: work possible. He especially wishes to express his gratitude to Professor F. G. Baender without

Lateral pulse jet control of a direct fire atmospheric rocket using an inertial measurement unit sensor system

Creator:: Jitpraphai, Thanat
Abstract:: Impact point dispersion of a direct fire rocket can be drastically reduced with a ring of appropriately sized lateral pulse jets coupled to a trajectory tracking flight control system. The system is shown to work well against uncertainty in the form of initial off-axis angular velocity perturbations as well as...
Resource Type:: Dissertation
Full Text:: . Abstract approved: Mark F. Costello Impact point dispersion of a direct fire rocket can be drastically

The impacts of ionization chemistry on hydrocarbon detonation

Creator:: Zaiger, Matthew F.
Abstract:: As carbon emissions are negatively impacting ecosystems across the globe, researchers are in a race against time to provide cleaner and more eÿcient power. Detonation engines can help meet the increasing demands for cleaner and more eÿcient power generation by providing an alternative means to use oxy-fuel combustion for carbon...
Resource Type:: Masters Thesis
Full Text:: = H+OH+ e 3.20× 1015 0.5 92,832 [48] 5 NO+ e = N+O+ e 1.05× 10−2 4.52 75,390 [46] 6 OH+ e = O+H+ e

An experimental and analytical study of the internal fluid dynamics of an ink-jet printhead

Creator:: Elger, D. F.
Resource Type:: Dissertation
Full Text:: the dimensionless dependent variables R/n/17, 6/0.85d1, vo/17;, and v 2 /v o were correlated with

ScholarsArchive@OSU

Repeated stress tests on carbon steels variously heat treated

The significance and measurement of the Tsai-Wu normal interaction parameter F₁₂

Practical application of steady-state 6-DoF aerodynamic model for vehicle system loads analysis

Design and construction of an improved conductor vibration recorder

Dynamic modeling, control and linear theory of a projectile equipped with a rotating internal part

Model predictive control of a direct fire projectile equipped with canards

An investigation of domestic oil heating with special emphasis on warm-air furnaces

Lateral pulse jet control of a direct fire atmospheric rocket using an inertial measurement unit sensor system

The impacts of ionization chemistry on hydrocarbon detonation

An experimental and analytical study of the internal fluid dynamics of an ink-jet printhead

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