NASA ISGC Fellowship
Application Deadline: March 7, 2025
NASA Idaho Space Grant Consortium 2025-2026 Graduate Fellowship.
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Each fellowship is worth $45,000 and is good for approximately one year.
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Eligibility: Applicants applying for an ISGC Fellowship must meet the following requirements:
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Must be a U.S. Citizen
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Must be enrolled in, or accepted into, a graduate degree program at an Idaho university.
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Must be enrolled as a full-time student
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Applications must be completed in NASA's STEM Gateway by March 7, 2025. The link to the application is: https://stemgateway.nasa.gov/s/course-offering/a0BSJ000001KiSX/isgc-20252026-fellowships
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Letters of Recommendation must be submitted to ISGC by March 7, 2025. Letters of Recommendation must be submitted via this link: https://app.smartsheet.com/b/form/3f2cda36bf254f07b6aff6a90be90d15
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An informational webinar will be held:
- Thursday, February 6 at 5:00 pm Pacific /6:00 pm Mountain
- Zoom Meeting Link: https://uidaho.zoom.us/j/83534699657
- A recording of the webinar will be posted
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If you have any questions, please email isgc@uidaho.edu
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2021-2022 Fellowship Awardees
Will Weygint
M.S., Department of Natural Resources and Society
University of Idaho
Rodrigo Padilla
Ph.D, Department of Mechanical Engineering
University of Idaho
Determining the suitability of thermal remote sensing for monitoring intra-annual tree growth in subalpine conifer forests of Idaho and the Intermountain West
Abstract:
Climate change-related shifts in hydrologic regimes are altering water availability in snowdominated ecosystems throughout Idaho and the Intermountain West. Of particular importance is increasing variability in the amount and duration of winter snowpack in subalpine forests and its
effects on tree wood growth, which provides important ecosystem services including wood production, habitat provisioning, and carbon sequestration. Due to its linkages to water availability tree wood growth could also be estimated using in-situ, airborne, and satellite leaf temperature measurements. The main goal of this project is to further explore linkages between tree wood growth and leaf temperatures to determine the suitability of using remotely sensed conifer shoot and canopy temperature (TS and TC, respectively) measurements as a proxy for intra-annual tree wood growth in subalpine forests. The two major objectives of this project are: 1) Explore feedbacks between TS and diurnal tree wood growth dynamics, and 2) test the spatial
scalability of the relationships between temperature and growth using unmanned aerial vehicle (UAV)-determined TC as well as satellite data products. This project will utilize in-situ data collected from an existing environmental monitoring network within the University of Idaho Nokes Experimental Forest near McCall, Idaho, as well as satellite TC measured from the ECOsystem Spaceborne Thermal Radiometer Experiment on Space Station (ECOSTRESS), a NASA instrument designed to collect surface temperature measurements across the globe. Results from this project will provide researchers and managers with a novel approach for monitoring the effects of climate change-induced alterations in hydrologic variability on tree wood growth in subalpine forests in Idaho and the Intermountain West. Idaho Space Grant Consortium Fellowship funding would be used to start this project and to complete analysis of objective 1 during the 2021-2022 academic year.
On the Aerodynamics of Fluid Structure Interaction
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Abstract:
An experimental study is being proposed to better understand flutter near the velocity instability range. Experiencing flutter is undesirable for aircraft in flight as it causes structural fatigue and failure, as well as contributing a large increase in drag. This phenomena will directly impact the efficiency of aircraft performance which is not desirable for the recent NASA project, Advanced Aerodynamic Design Center for Ultra-Efficient Commercial Vehicles. The scenario of ultra-efficient high-aspect wings is idealized to a cantilevered membrane to allow for a controlled experimental approach. Particle Image Velocimetry will be used to measure the velocity field that will be triggered along with load measurements experienced by the membrane on a corresponding time series. Hot Wire Anemometry will also be used to profile the wake of the membrane similarly be triggered with load measurements. This will allow to further quantify the pressure differential and the vortex shedding from a stable state to a uttering state. These measurements will help understand the causes of sudden flutter that will aid in validating models for these types of systems. Being able to understand these types of system will also help improve the design process for efficient aircrafts.