Aerodynamics Of A Supersonic Projectile In Proximity To A Solid Surface,
2010
University of New South Wales
Aerodynamics Of A Supersonic Projectile In Proximity To A Solid Surface, Graham Doig, Tracie Barber, Eddie Leonardi, Andrew J. Neely, Harald Kleine
Aerospace Engineering
Flow around a Mach 2.4 NATO 5.56 mm projectile in close proximity to a ground plane was investigated using computational fluid dynamics for a direct numerical reproduction of live-range experiments. The numerical approach was validated against both the live-range tests and subsequent wind-tunnel experiments. A nonspinning half-model and a full, spinning projectile were examined to clarify the influence of rotation. Multiple ground clearances were tested to obtain clear trends in changes to the aerodynamic coefficients, and the three-dimensional propagation and reflection of the shock waves were considered in detail. The behavior of the flow in the near wake was also …
Development Of Cubesat Vibration Testing Capabilities For The Naval Postgraduate School And Cal Poly San Luis Obispo,
2010
California Polytechnic State University, San Luis Obispo
Development Of Cubesat Vibration Testing Capabilities For The Naval Postgraduate School And Cal Poly San Luis Obispo, Marissa Brummitt
Master's Theses
The Naval Postgraduate School is currently developing their first CubeSat, the Solar Cell Array Tester CubeSat, or NPS-SCAT. Launching a CubeSat, such as NPS-SCAT, requires environmental testing to ensure not only the success of the mission, but also the safety of other CubeSats housed in the same deployer. This thesis will address the development of CubeSat vibration testing methodology at NPS, including subsystem testing, engineering unit qualification, and flight unit testing. In addition, the new Cal Poly CubeSat Test POD Mk III will be introduced and evaluated based upon comparison with the Poly Picosatellite Orbital Deployer (P-POD). Using examples from …
Thermal Models For A 3 Cm Miniature Xenon Ion Thruster,
2010
California Polytechnic State University, San Luis Obispo
Thermal Models For A 3 Cm Miniature Xenon Ion Thruster, Coleman Thomas Younger
Master's Theses
In order to support UCLA’s development of the 3 cm Miniature Xenon Ion (MiXI) thruster, Cal Poly has a 3 cm thruster under development. This version, called MiXI Cal Poly Version 1 (MiXI-CPv1), is complete and has been utilized in vacuum chamber thermal validation testing. Testing on this version was used to check the validity of heat transfer simulations modeled in SolidWorks. Investigations of the 3 cm ion thruster configuration were intended to discover the driving factors affecting the thermal behavior of the discharge chamber and surrounding design space.
Numerical simulations indicate that the heating of the samarium cobalt permanent …
Modeling Of A Gyro-Stabilized Helicopter Camera System Using Neural Networks,
2010
California Polytechnic State University, San Luis Obispo
Modeling Of A Gyro-Stabilized Helicopter Camera System Using Neural Networks, Nicholas Joseph Layshot
Master's Theses
On-board gimbal systems for camera stabilization in helicopters are typically based on linear models. Such models, however, are inaccurate due to system nonlinearities and complexities. As an alternative approach, artificial neural networks can provide a more accurate model of the gimbal system based on their non-linear mapping and generalization capabilities.
This thesis investigates the applications of artificial neural networks to model the inertial characteristics (on the azimuth axis) of the inner gimbal in a gyro-stabilized multi-gimbal system. The neural network is trained with time-domain data obtained from gyro rate sensors of an actual camera system. The network performance is evaluated …
Static And Fatigue Failure Response Of Woven Carbon Fiber Specimens With Double Edge Notches,
2010
California Polytechnic State University, San Luis Obispo
Static And Fatigue Failure Response Of Woven Carbon Fiber Specimens With Double Edge Notches, Ahmad J. Amini
Master's Theses
Carbon fiber composites are continually seeing increased use in aerospace applications. It is necessary to understand their failure modes in order to properly design and perform analysis on structures constructed primarily from them. This thesis studies woven carbon fiber composites with and without double-edge notches in a series of static and fatigue tests performed on an Instron 8801 servo-hydraulic testing system.
Specimens were constructed of Advanced Composites Group product # LTM45EL woven carbon fiber pre-preg/epoxy and were cut to approximately 9-inch in length and 1-inch in width. Notches were cut into some of the specimens using a slitting saw blade …
An Investigation Of Initially Delaminated Composite Sandwich With Delamination Arrest Mechanism Under Buckling Loading,
2010
California Polytechnic State University, San Luis Obispo
An Investigation Of Initially Delaminated Composite Sandwich With Delamination Arrest Mechanism Under Buckling Loading, Tony D. Tran
Master's Theses
This thesis involves the development of a fiberglass-foam composite sandwich structure with the introduction of delamination arrestment keys; therefore, a study of an initially delaminated composite sandwich structure was the experimental analysis on multiple configurations in how the arrestment keys are placed.
The first part of this thesis research was to the experimental design and manufacturing of the composite sandwich plates. These plates were later cut down to the specific test dimensions and manufacturing processes for the composite sandwich plates and test specimens were created. The composite sandwich plates were manufactured using a vacuum resin infusion process. The dimensions of …
Modeling And Simulation Of Autonomous Thermal Soaring With Horizon Simulation Framework,
2010
California Polytechnic State University, San Luis Obispo
Modeling And Simulation Of Autonomous Thermal Soaring With Horizon Simulation Framework, Zhenhua Li
Master's Theses
A thermal is a column of warm rising air triggered by differential heating on the ground. In recent studies UAVs were programmed to exploit this free atmospheric energy from thermals to improve their range and endurance. Researchers had successfully flown UAVs autonomously with thermal soaring method. Most research involved some form of flight simulation. Improvements to the aircraft and thermal models for simulation purpose would enable researchers to better design their UAVs and explore any potential flaws in their designs. An aircraft simulation with a thermal environment was created in Horizon Simulation Framework, a modeling and verification framework that was …
Bi-Material Attachment Through A Soft Tissue Interfacial System,
2010
Missouri University of Science and Technology
Bi-Material Attachment Through A Soft Tissue Interfacial System, Y. X. Liu, S. Thomopoulos, Victor Birman, J. S. Li, G. M. Genin
Mechanical and Aerospace Engineering Faculty Research & Creative Works
No abstract provided.
The Next Generation Cubesat: A Modular And Adaptable Cubesat Frame Design,
2010
California Polytechnic State University - San Luis Obispo
The Next Generation Cubesat: A Modular And Adaptable Cubesat Frame Design, James Dolengewicz, Lucas Whipple, Stephanie Wong
Mechanical Engineering
The goal of this project is to develop an improved next-generation CubeSat structure for Cal Poly’s PolySat program. Notable achievements include significantly increased ease of access, design to optimize payload space, improved machinability, increased modularity and a platform which allows for easy integration of future payloads.
2-D Path Planning For Direct Laser Deposition Process,
2010
Missouri University of Science and Technology
2-D Path Planning For Direct Laser Deposition Process, Swathi Routhu, Divya Kanakanala, Jianzhong Ruan, Xiaoqing Frank Liu, Frank Liou
Computer Science Faculty Research & Creative Works
The zigzag and offset path have been the two most popular path patterns for tool movement in machining process. Different from the traditional machining processes, the quality of parts produced by the metal deposition process is much more dependent upon the choice of deposition paths. Due to the nature of the metal deposition processes, various tool path patterns not only change the efficiency but also affect the deposition height, a critical quality for metal deposition process. This paper presents the research conducted on calculating zigzag pattern to improve efficiency by minimizing the idle path. the deposition height is highly dependent …
Hot Air Balloon Navigation,
2010
California Polytechnic State University, San Luis Obispo
Hot Air Balloon Navigation, Dustin Blackwell
Aerospace Engineering
This report describes a program used for navigating a hot air balloon. The program, Balloon_Trip, was written using MATLAB and gives a flight path to follow from a start position to an end position. Balloon_Trip calculates the flight path by taking in wind conditions and then flying through these different winds so as to steer the hot air balloon. The program calculates the flight path by taking into consideration at all times how the wind will propel the balloon while it is rising or falling in elevation. It then takes the most direct and least complicated, if not fastest, …
The Effectiveness Of Damage Arrestment Devices In Delaying Fastener-Hole Interaction Failures In Carbon Fiber Polyurethane Foam Composite Sandwich Panels Subjected To Static And Dynamic Loading Under Increased Temperatures,
2010
California Polytechnic State University, San Luis Obispo
The Effectiveness Of Damage Arrestment Devices In Delaying Fastener-Hole Interaction Failures In Carbon Fiber Polyurethane Foam Composite Sandwich Panels Subjected To Static And Dynamic Loading Under Increased Temperatures, Dominic E. Surano
Master's Theses
A study was conducted to investigate simple, cost-effective manufacturing techniques to delay skin-core delamination, micro-buckling and bearing stress failures resulting from fastener-hole interactions. Composite sandwich panels, with and without damage arrestment devices (DADs), were subjected to monotonic compression at a rate of 5mm per second, and compression-compression fatigue at 50% yield at an amplitude of 65%, under temperatures of 75, 100, 125, 150, 175, and 200 °F.
The sandwiches tested were composed of two-layer cross-weave carbon fiber facesheets, a polyurethane foam core, and an epoxy film adhesive to join the two materials. The most successful method to delay the aforementioned …
A 24ft/7.3m Parabolic Reflector Antenna Performance & Feed Design Analysis,
2010
Morehead State University
A 24ft/7.3m Parabolic Reflector Antenna Performance & Feed Design Analysis, Anthony Shelley
Morehead State Theses and Dissertations
A thesis presented to the faculty of the College of Science & Technology at Morehead State University in partial fulfillment of the requirements for the Degree of Master of Science by Anthony Shelley on November 29, 2010.
The Weather Forecast Fortoday In Space! Exploring Our Space Environment & Satellite Orbits,
2010
Morehead State University
The Weather Forecast Fortoday In Space! Exploring Our Space Environment & Satellite Orbits, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint presentation created by Professor Bob Twiggs titled "The Weather Forecast forToday in Space! Exploring our space environment & satellite orbits" from November 17, 2010.
Descent Systems For An Improved And Reusable Gemini Capsule,
2010
University of Alabama in Huntsville
Descent Systems For An Improved And Reusable Gemini Capsule, Heather Pitts
Von Braun Symposium Student Posters
No abstract provided.
Nasa X-Toolss Design Optimization,
2010
University of Alabama in Huntsville
Nasa X-Toolss Design Optimization, David Keeton, Cheryl Rose, Daniel Cervantes, Kelly Green, Justin Chism
Von Braun Symposium Student Posters
No abstract provided.
Aethon Research Rocket, Charger Rocket Works,
2010
University of Alabama in Huntsville
Aethon Research Rocket, Charger Rocket Works, Daniel Cavender, Diana Alsbrook, Leonard French, Jarred Green, Andrew Hiatt, Jarrod Mosteller, Brandon Setayesh, Nathan Toy
Von Braun Symposium Student Posters
No abstract provided.
Mars Sample Return Utilizing The Capabilities Of The Heavy Lift Launch Vehicle,
2010
University of Alabama in Huntsville
Mars Sample Return Utilizing The Capabilities Of The Heavy Lift Launch Vehicle, Matt White
Von Braun Symposium Student Posters
No abstract provided.
Design And Fabrication Of A 1/3 Scale Gemini-Style Capsule,
2010
University of Alabama in Huntsville
Design And Fabrication Of A 1/3 Scale Gemini-Style Capsule, Toshawnka Walker, Jonathan Davis, Brockton Thompson, Ryohsuke Aoki
Von Braun Symposium Student Posters
No abstract provided.
Poias Philoctetes/Okyrhoe Integrated Asteroid Surveyor,
2010
University of Alabama in Huntsville
Poias Philoctetes/Okyrhoe Integrated Asteroid Surveyor, Ian Maddox
Von Braun Symposium Student Posters
No abstract provided.
