Browsing by Author "Jacob, Jamey"
Now showing items 1-20 of 47
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Aerodynamics of active and passive dispersal of miniature insects with bristled wings
Kasoju, Vishwa Teja (2021-07)Tiny insects with body lengths under 2 mm, such as thrips, use fringed/bristled wings for active flapping at Reynolds number (Re) on the order of 10. Even at such tiny scales these insects were found to fly effectively ... -
Applying satellite remote sensing, unmanned systems, and models for water quality analysis
Pamula, Abhiram Siva Prasad (2022-07)Transport of soils and sediment by runoff diminish the surface water quality of lakes/reservoirs and shrink reservoir capacity. Nutrients move with transported soil and sediment due to soil erosion by floods and high wind. ... -
Automated Dynamic Propeller Testing At Low Reynolds Numbers
Gamble, Dustin Eli (Oklahoma State University, 2009-12-01)Experiments were conducted on small propellers using a motor dynamometer in a wind tunnel. The effects at different Reynolds number were observed. To maintain Reynolds number and consistent test procedures, the wind tunnel ... -
Characterization of the impulsive jet produced from a dolphin's blowhole
Barton, C. J. (2020-12)The health of bottlenose dolphins can be monitored by marine biologists through the analysis of their exhaled breath. Unique concepts to capture this breath in the wild include flying an Unmanned Aerial System (UAS) through ... -
Computational fluid dynamics study for stability analysis of an unmanned aircraft mass simulator with rocket-assisted take-off
Totty, Christopher D. (2022-05)This paper presents the stability analysis of a high speed unmanned aerial system mass simulator fitted with a rocket-assisted take-off (RATO) system. Flight stability characteristics from rocket ignition to rocket burnout ... -
Coolant passage segmentation influence on regenerative-cooling effectiveness for small spacecraft thrusters
Utley, Lucas (2020-05)The purpose of this thesis is to examine the effect of varying the number of cooling passages in a regeneratively-cooled rocket combustion chamber and nozzle analog for a small spacecraft thruster producing 22N (5lbf) ... -
Deployment Dynamics of Inflatable Wings
Loh, Weng Kheong (Ben) (Oklahoma State University, 2008-12-01)Dynamic deployment of inflatable wings were investigated through laboratory, wind tunnel and flight testing. The goal of the research is to design an in-flight morphing wing aircraft using semi-span inflatable wings that ... -
Design and control of a spherical VTOL vehicle
Loh, Weng Kheong (Ben) (2019-12)This research presents the design of a spherically shaped Unmanned Aircraft System (UAS) called the All-Terrain Land and Air Sphere (ATLAS). ATLAS is designed to include competing design requirements necessary for operating ... -
Design and Development of a 3D Printed UAV
Banfield, Christopher P. (2015-07-01)The purpose of this project was to investigate the viability and practicality of using a desktop 3D printer to fabricate small UAV airframes. To that end, ASTM based bending and tensile tests were conducted to assess the ... -
Design and development of a tornado intercept unmanned aerial vehicle
Ross, Andrew Levi (2019-12)Very little data surrounding tornado genesis exists, and this is due in part to the lack of tools necessary to deliver weather-sensing instruments into the severe weather phenomenon. Though current UAS are able to accurately ... -
Design and evaluation of a thermal nozzle for small-scale turbojets
Braun, Joshua Robert (2022-05)This paper presents the design and evaluation of a thermal nozzle for small-scale turbojets. Historically, small-scale turbojets have suffered from poor thermal efficiency and thrust specific fuel consumption (TSFC). This ... -
Design, analysis, and integration of a turboelectric propulsion and power system for unmanned aircraft
Moody, Kylar Julian (2020-05)Electrically powered small unmanned aerial systems face limited range and endurance due to the inherently low energy density of current level of technology batteries. Hybrid gas-electric systems are under development and ... -
Development of a dolphin hormone sample collection device for UAS
Abele, Eric (2021-07)Marine biologists are able to quantify the stress in dolphins through analysis of hormones in mucus samples released from the blowhole while breathing. This method provides a noninvasive approach compared to current methods ... -
Development of a Microgravity Uas Test Bed
Hathaway, Jacob Derk (2016-07-01)The ultimate goal is to develop a vehicle that can produce a microgravity environment for space system research within a small to medium sized UAV. This weight class of vehicle provides a platform that is more available ... -
Development of a Microsoft Excel Based Uav Propeller Design and Analysis Tool
Lowe, Trevor Edwin (2015-12-01)QPROP/QMIL were developed by Professor Mark Drela at MIT for use in designing propellers and windmills for various flow conditions. These tools have been used by other graduate students with varying degrees of success, ... -
Effects of electrode material on electrode erosion of electrical discharge machining drill
Copher, Garner (2021-05)This paper presents an experimental investigation of the effects of electrode material and workpiece material on electrode wear and performance of a handheld electrical discharge machining drill. In the aerospace maintenance, ... -
Evaluation of a dual-mode, turbojet-turboprop engine for unmanned aircraft
Schinzler, Trey (2022-05)This paper provides experimental feedback on the feasibility of a small-scale, dual-mode turbojet to turboprop engine. The engine used for testing was a KingTech K45-TP. Key parameters focused on for this experiment were ... -
Evaluation of granular distribution and propellant grain length on tri-modal ammonium perchlorate solid rocket motors
Velasco, Daniel (2022-05)This paper presents an evaluation on the effects that variances in ammonium perchlorate particles size, total aluminum content ratio, and solid rocket motor geometry has on tri-modal ammonium perchlorate composite solid ... -
Experimental and Computational Investigation of the Conformal Vortex Generator
Kibble, Geoffrey Alexander (2017-08-01)Passive flow control devices, such as vortex generators or riblets, have limited applications and often provide benefits with the expense of drag or increased cost. Many flow control methods have come and gone due to the ... -
Finite element analysis for the design of novel ceramic propellers
Harmon, Katelynn (2022-12)Ceramics are stiff, lightweight and less prone to deflection. However, ceramics have not historically been used in propeller applications. Little is known about how ceramics will react to the various loading situations of ...