Matching Items (3)
Description
This thesis outlines the creation of an excel tool designed to utilize public flight data for a given flight and determine further information such as general flight properties, weight estimation, and aerodynamic and stability characteristics. In depth analyses is done for a TV Relay flight of a Beechcraft Super King Air 200 to display the data processing and accuracy of the values. From this analyses it is displayed that the aircraft is flown safely and well within its performance parameters for the entire mission. The usefulness of this tool comes from its ability to successfully analyze critical properties and perform pilot and crash reconstruction analysis.
ContributorsSchierbrock, Aaron James (Author) / Takahashi, Timothy (Thesis director) / Niemczyk, Mary (Committee member) / Mechanical and Aerospace Engineering Program (Contributor, Contributor) / Barrett, The Honors College (Contributor)
Created2020-05
Description
The alarming decline of insect pollinators is due in part to agrochemical exposure and climate warming. This thesis focuses on understanding how exposure to a commonly used fungicide and high air temperature affect the flight behavior and physiology of the very important commercial pollinator, Apis mellifera. I found that honey bees reared on pollen contaminated with field-realistic levels of a fungicide (Pristine®) commonly applied to almond blossoms before pollination had smaller thoraxes, possibly due to inhibition of protein digestion, plausibly reducing flight capability. By flying unloaded bees in low density air to elicit maximal performance, I found that consumption of high doses of fungicide during development inhibited maximal flight performance, but consumption of field-realistic doses did not.
To understand climatic-warming effects on honey bees, I flew unloaded foragers at various air densities and temperatures to assess the effects of flight muscle temperature (29 to 44°C) on maximal aerobic metabolism. Flight metabolic rate peaked at a muscle temperature of 39°C and decreased by ~2% per degree below and ~5% per degree above this optimum. Carrying nectar loads increased flight muscle temperatures and flight metabolism of foragers flying at air temperatures of 20 or 30°C. Yet, remarkably, bees flying at 40°C were able to carry loads without heating up or increasing metabolic rate. Bees flying at 40°C increased evaporative cooling and decreased metabolic heat production to thermoregulate. High speed video revealed that bees flying at 40°C air temperature lowered their wing beat frequency while increasing stroke amplitude, increasing flight efficiency. My data also suggests that cooler bees use wing kinematic strategies that increase flight stability and maneuverability while generating excess heat that warms their flight muscle toward optimum. High water loss rates during flight likely limit foraging in dry air temperatures above 46°C, suggesting that CTmax measures of resting honey bees significantly overestimate when high air temperature will negatively impact flight and foraging.
ContributorsGlass, Jordan Robert (Author) / Harrison, Jon F. (Thesis advisor) / Denardo, Dale F. (Committee member) / Dudley, Robert (Committee member) / Fewell, Jennifer H. (Committee member) / Arizona State University (Publisher)
Created2023
Description
The objective of this study is to estimate the variation of flight performance of a variable sweep wing geometry on the reverse engineered Boeing 2707-100 SST, when compared against the traditional delta wing approach used on supersonic airliner. The reason for this lies beneath the fact that supersonic orientations of wings doesn’t seem to work well for subsonic conditions, and subsonic wings are inefficient for supersonic flight. This would likely mean that flying long haul subsonic with supersonic wing geometry is inefficient compared to regular aircraft, but more importantly requires high takeoff/landing speeds and even long runways to bring the aircraft to hold. One might be able to get around this problem - partially - by adding thrust either by using afterburners, or by using variable geometry wings. To assess the flight performance, the research work done in this report focuses on implementing the latter solution to the abovementioned problem by using the aerodynamic performance parameters such as Coefficient of Lift, Coefficient of Drag along with its components specific to every test Mach number and altitude, along with the propulsion performance parameters such as thrust and thrust specific fuel consumption at different iterations of power settings of engine, flight Mach number and altitude in a propulsion database file to estimate flight performance using flight missions and energy-maneuverability theory approach. The flight performance was studied at several sweep angles of the aircraft to estimate the best possible sweep orientation based on the requirement of mission and an optimal flight mission was developed for an aircraft with swing wing capabilities.
ContributorsChaudhari, Bhargav Naginbhai (Author) / Takahashi, Timothy T (Thesis advisor) / Dahm, Werner J (Committee member) / Kim, Jeonglae (Committee member) / Arizona State University (Publisher)
Created2021