Jonathan Raush

Dr. Jonathan Raush

orcid

Research Focus & Metrics

Academic Career Length

6Years (2021-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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20 May 2022 in Materials
Verified
Journal Article
Open access
PDF file
Congyuan ZengCongyuan Zeng
Congyuan Zeng
HGHamed Ghadimi
Hamed Ghadimi
Huan DingHuan Ding
Huan Ding
SNSaber Nemati
Saber Nemati
AGAbdelrahman Garbie
Abdelrahman Garbie
SGShengmin Guo
Shengmin Guo
In this paper, the phase structure, composition distribution, grain morphology, and hardness of Al6061 alloy samples made with additive friction stir deposition (AFS-D) were examined. A nearly symmetrical layer-by-layer structure was observed in the cross section (vertical with respect to the fabrication-tool traversing direction) of the as-deposited Al6061 alloy samples made with a back-and-forth AFS-D strategy. Equiaxed grains were observed in the region underneath the fabrication tool, while elongated grains were seen in the “flash region” along the mass flow direction. No clear grain size variance was discovered along the AFS-D build direction except for the last deposited layer. Grains were significantly refined from the feedstock (~163.5 µm) to as-deposited Al6061 alloy parts (~8.5 µm). The hardness of the as-fabricated Al6061 alloy was lower than those of the feedstock and their heat-treated counterparts, which was ascribed to the decreased precipitate content and enlarged precipitate size.

19 May 2024 in Scripta Materialia
Verified
Journal Article
Open access
GSGloria A Sulley
Gloria A Sulley
JRJonathan Raush
Jonathan Raush
MMMatthew M. Montemore
Matthew M. Montemore
JHJihun Hamm
Jihun Hamm

7 May 2022 in Energies
Verified
Journal Article
Open access
PDF file
DKDEEPAK JAIN VEERENDRA KUMAR
DEEPAK JAIN VEERENDRA KUMAR
LDLelia Deville
Lelia Deville
KIK Ritter III
K Ritter III
JRJonathan Raush
Jonathan Raush
FFFarzad Ferdowsi
Farzad Ferdowsi
TCTerrence Chambers
Terrence Chambers
In this work, performance analysis and comparison of three photovoltaic technologies are carried out in the Louisiana climate. During the calendar year of 2018, the University of Louisiana at Lafayette constructed and commissioned a 1.1 MW solar photovoltaic power plant for researching solar power in southern Louisiana and for partial energy demand of the university. It was one of the largest solar photovoltaic power plants in Louisiana when constructed and receives an annual solar insolation of 4.88 kWh/m2/d at latitude minus five degrees (25°) tilt. The solar power plant has a total of 4142 modules and incorporates three module technologies. Preliminary performance data from the system level are presented. The evaluation of different technologies is based on final yield, performance ratio, and capacity factor for one year from September 2019 to August 2020. An economic analysis is carried out using levelized cost of energy for the three photovoltaic (PV) technologies. Finally, the results are compared with simulated results of System Advisor Model (SAM) and PVsyst. It was found that copper indium gallium selenide (CIGS) has better performance ratio of 0.79 compared with monocrystalline silicon and polycrystalline silicon, which have performance ratios of 0.77 and 0.73, respectively. The simulation results correlated with the actual performance of the plant.

14 April 2022 in Energies
Verified
Journal Article
Open access
PDF file
JWJoshua A Wilson
Joshua A Wilson
YWYudong Wang
Yudong Wang
JCJohn Carroll
John Carroll
JRJonathan Raush
Jonathan Raush
GAGene Arkenberg
Gene Arkenberg
XZXiao-Dong Zhou
Xiao-Dong Zhou
A thermodynamic model was developed and validated to analyze a high-performance solid oxide fuel cell and gas turbine (SOFC-GT) hybrid power system for electric aviation. This study used a process simulation software package (ProMax) to study the role of SOFC design and operation on the feasibility and performance of the hybrid system. Standard modules, including compressor, turbine, heat exchanger, reforming reactor, and combustor were used from the ProMax tool suite while a custom module was created to simulate the SOFC stack. The model used an SOFC test data set as an input. Additional SOFC stack performance effects, such as pressure, temperature, and utilization of air and fuel, were added from open source data. System performance predictors were SOFC specific power, fuel-to-electricity conversion efficiency, and hybrid system efficiency. Using these input data and predictors, a static thermodynamic performance model was created that can be modified for different system configurations and operating conditions. Prior to creating the final aircraft performance model, initial demonstration models were developed to validate output results. We used the NASA SOFC model as a benchmark, which was created with their Numerical Propulsion System Simulator (NPSS) software framework. Our output results matched within 1% of both the NASA model and open source SOFC performance data. With confidence gained in the accuracy of this model, a 1-MW SOFC-GT hybrid power system was constructed for an aircraft propulsion concept. Overall hybrid system efficiencies of > 75% FTE were observed during standard 36,000 feet cruise flight conditions.

1 April 2021 in Manufacturing Letters
Verified
Journal Article
Closed access
CZCongyuan Zeng
Congyuan Zeng
HWHao Wen
Hao Wen
BBBenjamin C. Bernard
Benjamin C. Bernard
JRJonathan Raush
Jonathan Raush
Paul GradlPaul Gradl
Paul Gradl
SGShengmin Guo
Shengmin Guo

4 January 2023 in Materials
Verified
Journal Article
Open access
PDF file
HGHamed Ghadimi
Hamed Ghadimi
AJArash Pourbagheri Jirandehi
Arash Pourbagheri Jirandehi
SNSaber Nemati
Saber Nemati
Huan DingHuan Ding
Huan Ding
AGAbdelrahman Garbie
Abdelrahman Garbie
SGShengmin Guo
Shengmin Guo
In this paper, small blocks of 17-4 PH stainless steel were manufactured via extrusion-based bound powder extrusion (BPE)/atomic diffusion additive manufacturing (ADAM) technology in two different orientations. Ultrasonic bending-fatigue and uniaxial tensile tests were carried out on the test specimens prepared from the AM blocks. Specifically, a recently-introduced small-size specimen design is employed to carry out time-efficient fatigue tests. Based on the results of the testing, the stress–life (S-N) curves were created in the very high-cycle fatigue (VHCF) regime. The effects of the printing orientation on the fatigue life and tensile strength were discussed, supported by fractography taken from the specimens’ fracture surfaces. The findings of the tensile test and the fatigue test revealed that vertically-oriented test specimens had lower ductility and a shorter fatigue life than their horizontally-oriented counterparts. The resulting S-N curves were also compared against existing data in the open literature. It is concluded that the large-sized pores (which originated from the extrusion process) along the track boundaries strongly affect the fatigue life and elongation of the AM parts.