暗网禁区破解版

Aerospace engineers design high-performance systems, including aircraft, spacecraft, satellites and missiles. They have an understanding of aerodynamics, flight mechanics, structures and propulsion. Our graduates work in analysis/design and research/development for local, national and international companies and organizations.

2025 Senior Design Projects

Aces Aerospace鈥檚 Solution for Urban Scientific Sample Transportation

MEMBERS: Erik Andersen , Lucas Baker, Derek Eitzmann, Tracey Hill , Zach Silvis

ADVISOR: Dr. Jielong Cai

SPONSOR: Boeing

Aces Aerospace has developed a half-scale model for a cutting-edge unmanned short takeoff and landing (STOL) aircraft that is designed to address the logistical challenge of transporting scientific samples from both remote and urban environments. Our team aims to solve this issue by providing an aircraft engineered with long-range, high payload capacity, and a minimal runway requirement. This enables our aircraft to serve several industries such as medical research, environmental monitoring, and emergency response. Aces Aerospace interviewed a research professor with 暗网禁区破解版 Geology, a strategic partnership manager at NASA, and a special agent with the FBI. Based on these interviews, a list of real-world payloads could include water samples, geological samples, forensic evidence, and medical specimens. Our aircraft can provide faster access to critical data by having equipment on board that can begin sample analysis, producing results such as identification of bacterial pathogens in water, composition of rock samples, blood type from a crime scene sample, or viral infection identification on a test sample. An additional benefit of our aircraft is its compact frame, roughly the width of an SUV, allowing the aircraft to maneuver in tight areas and land on single-lane roads within 30ft. Furthermore, the unmanned small-scale design allows the customer to receive the same benefits as a full-scale aircraft at a much lower purchase price with lower operational costs. In summary, the Aces Aerolink provides the perfect solution for scientific sample transportation by providing fast access to critical data while being versatile enough to tackle any terrain. 

AEMS (Aerial Emergency Medical Suppliers) 

MEMBERS: Brody Hendrich, Nicholas Janzen, Radeef Karim, Connor O'Neill, John Cummings

ADVISOR: Dr. Jielong Cai

SPONSOR: Boeing

Delivering emergency medical supplies promptly during high traffic or natural disasters becomes almost impossible. Patients and EMS personnel require lifesaving interventions as soon as possible. Mach Street Boys aims to deliver these crucial supplies to those in need via Urban Air Mobility, known as Aerial Emergency Medical Suppliers (AEMS). Mach Street Boys is committed to easy accessibility and ensures that deliveries reach all destinations swiftly. AEMS will be a full-scale product capable of holding a payload that will ultimately be delivered to the desired location. What makes AEMS unique is its ability to maneuver urban environments more efficiently than other transportation aircraft required to unload at specific locations. The AEMS aircraft can take off and land from a shorter runway, making it ideal to fly in and out of tight spaces to deliver essential supplies.

AeroFIN Barracuda: A STOL Aircraft for Delivery of Power to Disaster Affected Areas

MEMBERS: Treyton Blecke, Luke Cotter, Diego Fuentealba, Aiden Holt, Kaishi Kawakami

ADVISOR: Dr. Jielong Cai

SPONSOR: Boeing

An often-overlooked part of disaster relief is the need for power and internet service. A wide array of natural disasters can cause power and Wi-Fi outages. Disasters such as hurricanes, earthquakes, tornadoes, snowstorms, sandstorms, wildfires, and even heat waves and extreme cold can over-stress power grids. Many companies and humanitarian groups focus on the delivery of medical equipment, food, water, and other humanitarian aid. While such aide is critical, it does not help important infrastructure like hospitals, water plants, and waste processing plants maintain power. Additionally, large swaths of the population are often left without the power needed to run their refrigerators, heating and cooling units, medical equipment, and other power-dependent equipment. They may be left without internet connectivity, leaving them unable to receive important updates from officials, call for help, or check on family members and friends. Therefore, an aircraft that can provide power and internet connectivity equipment for urban areas affected by natural disasters, such as generators, gas, oil, batteries, satellite internet router-modems, solar panels, and battery powered/crank radios, has been designed. The aircraft utilizes short take-off and landing capabilities to perform maneuvers and reach areas in critical conditions that other vehicles/aircraft are unable to reach. With this ability, this plane can support urban areas in need.

Air Tourism with Meadowlark Views 

MEMBERS: Francisco Murillo, Lanie Mott, Christopher Montford, Allinsipas Montoya

ADVISOR: Dr. Jielong Cai

SPONSOR: Boeing

Meadowlark Views is a STOL UAV that will conduct air tourism routes in picturesque skyline cities. The purpose of this aircraft will be to carry a customer鈥檚 phone for them to experience the city through their camera. To achieve this STOL mission, Meadowlark Views will take off from a short 16-foot elevated runway, fly around the Heskett Center second-floor gym, land on a 50-foot runway, fly again, and then land on the 16-foot elevated runway. To take off from the short 16-foot runway, the team will utilize flaps that provide additional lift and a three-bladed 11x7E propeller to reach take-off speed within the runway length. During flight time, the aircraft will rely on its US-35B airfoil to generate enough lift to fly at a cruise speed of about 35 ft/s. Additionally, Meadowlark Views will use its aileron, rudder, and elevator control surfaces to maneuver around the tight corners of the Heskett gym which will simulate the small enclosed spaces of an urban region. Finally, to land, the team will use the flaps again to act like spoilers to provide more drag for the plane to slow down to a stop within 16 feet. The completion of this mission will result in an enjoyable flight experience for the customers to experience through their phones. 

Airborne Scout

MEMBERS: Jordan Glover, Caleb McDaniel, Marion Jackson, Celestino Almeida

ADVISOR: Dr. Jielong Cai

Our mission is to assist the ariel surveillance sector by providing an ariel platform that is cost effective, easy to manufacture, and easy to integrate into their daily operations.

The design is to emulate a surveillance operation in which the aircraft will takeoff, perform an aerobatic maneuver, land for payload pickup, and then return to the maneuvering phase before final landing.  

De-Icer 1: Safe Winter Travel via Aerial De-Icing

MEMBER: Darsh Choksi, Kody Sudol, Laura Santos, Phanindar Pokala, Tyler Shuford

ADVISOR: Dr. Jielong Cai

SPONSOR: Boeing

Each year, 24 percent of weather-related vehicle accidents occur on icy, slushy, or snowy conditions, accounting for over 116,800 injuries in the United States [1]. Current ground road maintenance is time consuming and dangerous. By taking advantage of the growing Urban Air Mobility (UAM) market, STARFLEET introduces the DE-ICER 1 aircraft as a key solution to address winter transportation challenges. The De-Icer 1 is an eco-friendly electric aircraft made with composite materials; designed for precise aerial delivery of de-icing agents onto bridges. With its short takeoff and landing (STOL) capabilities, it may be deployed from the heart of a city- such as a rooftop, reaching critical areas faster than snow trucks. With this solution, drivers will not have to face the dangerous conditions that bridges present in icy/snowy conditions. State governments may benefit from reducing salt overuse which harms the environment, minimizing road closures and improving efficiency of de-icing procedures within cities. The De-Icer 1 offers a simple design so that design changes may easily be made to fit various use cases, enabling off-season functionalities-all while being eco-friendly and cost efficient. This airplane has the power to transform city-wide road safety as we know it, reducing accidents, saving lives and minimizing its carbon footprint. 

[1] National Weather Service.

 

Prototype Eagles

MEMBERS: Jacob Mohlman, Jance Wehkamp, Oscar Fernandez, Logan Janes, Antonio Rojas

ADVISOR: Dr. Suresh Keshavanarayana

This project focuses on the design, construction, testing, and successful flight of a custom built aircraft. A primary goal was to integrate the major areas of aerospace engineering principles (Aerodynamics, Flight Dynamics and stability, Structural Analysis, and Propulsion systems) to develop not only a functional aircraft, but one designed to a specific goal to meet mission criteria. The team started with a conceptual design followed with iterations of detailed simulations, analyses, and eventually a detailed, finalized design. After the construction of the aircraft, the team conducted a series of structural and wind tunnel testing to verify or modify certain characteristics impeding stability about the aircraft. The team then took to the skies to showcase their valuable work and dedication to the aerospace field of study. This project provided invaluable experience in applying a growth of knowledge to a practical, real world, engineering setting. It used teamwork, patience, problem solving, and innovation to overcome the challenges of aircraft design and testing.

Scrambled Jets - Aerospace Design Team 6

MEMBERS: Nicholas Inzerillo, Andres Erives, Nathan Atkison, Jospeh Melero

ADVISOR: Dr. Jielong Cai

Short takeoff and landing aircraft (STOL) can fly a wide variety of missions in urban settings. One mission that stood out was the transportation of medical items between hospitals in dense urban areas. It was decided to build a STOL aircraft that is capable of takeoff from a hospital roof with fragile pharmaceutical supplies. These supplies would be air dropped onto the roof of another hospital. The glass eggs being transported mimic the fragile pharmaceutical supplies the aircraft would need to transport in the real applications. 
Currently, hospitals use ground vehicles to transport pharmaceutical supplies between hospitals. While these vehicles can get the job done, they are prone to delays due to road conditions such as traffic and construction making them less ideal for patients in critical condition. Aircraft can completely bypass road conditions and take a straight route to the hospital. 

Senior Design Project

MEMBERS: Kubeshavarsha Kalithasan, Anubhav Pant, Pedro Cordeiro Povoa Cupertino, Ami Goto, Yuto Minami

ADVISOR: Dr. Jielong Cai

This work-in-progress paper presents the design of a Short Takeoff and Landing (STOL) Unmanned Aerial Vehicle (UAV) equipped with a modular cargo system, developed by undergraduate engineering students. The UAV aims to support versatile operations in urban, remote, and disaster-stricken areas through an adaptable, easily deployable platform. 

Designed for the Boeing Propeller Bronze Competition, the project integrates key engineering education practices, including Project-Based Learning (PBL), Model-Based Engineering (MBE), and Quality-Cost-Delivery (QCD) analysis. These methodologies guided the team in tackling a real-world aerospace challenge using formal engineering processes.

Initial sizing was achieved through constraint diagrams and weight estimation models, while the MBE Diamond Framework provided a structured approach covering need analysis, behavior modeling, system architecture, and design verification. Various CAD-based configurations were modeled and analyzed using 3DEXPERIENCE, allowing the team to evaluate manufacturability and flight performance under mission constraints.

The resulting design features a bi-wing layout with a cartridge-style modular cargo bay. It meets competition constraints, including a maximum weight of 4 pounds and a takeoff distance under 16 feet. The project also remained within a $600 budget, balancing cost, performance, and ease of manufacturing.

SOAR Plane - Safe Organ Air Relay

MEMBERS: Sarah Varner, Nate Scarrow, Paige Nobles

ADVISOR: Dr. Jielong Cai

The team was tasked with defining a unique, valuable mission statement for the plane they designed and built. Recognizing Wichita's needs in the medical field and the various hospitals spread across the metro area and even rural Kansas, the team made a small-scale, unmanned, fixed-wing aircraft to transport and pick up organs needed for medical transplants in a secure, fast manner. The plane can take off from a short platform (a hospital helipad, for example), and fly to where the organs are located. When the plane arrives, it picks up and transports organs to another hospital via helipad or any available runway surface that is available, via cushioned, air-tight, climate-controlled, and sterile containers. This is a unique solution in the way that pilots would not be necessary for transporting the organs, and it is electric powered, saving money on fuel and labor, as well as making the aircraft lighter. By avoiding the need to drive on roads or through traffic, this plane significantly reduces the time needed to transport lifesaving organs and improves the chances of successful transplants.

SpaceY - The Robot Chicken

MEMBERS: Julia McLaughlin, Hunter Robertson, Zachary Oakley, Jason Hildreth

ADVISOR: Dr. Jielong Cai

In the realm of Urban Air Mobility (UAM), almost every company is vying to be the best at transporting 1-4 people. While this may be an effective method to help relieve the issues with current urban transportation methods, it raises concerns about creating similar problems in the air. SpaceY presents the Robot Chicken, an electric STOL aircraft designed to take off and land in less than 15 feet, corresponding to a full scale runway of roughly 300 feet, around 6% the length of a traditional runway! Designed for efficiency, manufacturability, and repairability, this aircraft can transport 16 passengers from a rural area into a city and back as a means of daily transport reducing the number of vehicles on the road while simultaneously reducing carbon emissions. The unique lifting body fuselage maintains a lightweight and efficient profile and the modular design makes for easy disassembly for repairs and a compact form factor for ground transport. Alternate interior configurations of this aircraft also support the relocation of people, supplies and equipment during natural disasters where ground transportation is interrupted, unmanned military transport, aerial tourism, and evacuation from war zones where the established humanitarian corridors for civilians are not being properly observed. 

SS-25 Soaring Sterling, a Solution to Urban Area Power Outages

MEMBERS: Mason Hensley, Joseph Macko, Caleb Perkins, Zephan Rodriguez, Peter Stuhlsatz

ADVISOR: Dr. Jielong Cai

In recent years, power grids in highly dense urban populations have been susceptible to long-term outages due to extreme weather. Many highly dense cities do not have the infrastructure to maintain power during these anomalies. The same can be said in war-torn regions where conflicts severely limit the ability to produce sustained power. These power disruptions not only affect households but also cripple critical infrastructure like hospitals, communication networks, and transportation systems. In times of large-scale outages, the military does not currently possess the manpower and machinery necessary to support power outages in highly dense urban populations 

That is where the SS-25 Soaring Sterling fills this need in power restoration and sustainment by delivering necessary equipment and technicians to areas in need and supplying power until the region鈥檚 power grid can return online. The SS-25 is an Urban Air Mobility aircraft capable of short take-offs and landings on asphalts or on rough terrain. The SS-25 has the maneuverability and endurance necessary to fly through a highly dense urban environment to an area in need. SS-25 is meant for short notice operations with its automatic loading of a modular cargo container picking up containers such as generators underneath the belly of the aircraft. The SS-25 carrying a large payload would be a certified aircraft underneath the FAA鈥檚 Code of Federal Regulations as a Part 25 aircraft. 

Stop by our booth to see the flight-tested RC aircraft prototype and try flying our aircraft in the flight simulator! 

 

2025 (Non-Senior Design) Undergraduate Projects

Application of Magnus Effect in Improving Aircraft Landing and Takeoff Performance

MEMBERS: Caden Carlson, Gary Tran, Reese Pekny, Will Fischer

ADVISOR: Dr. Vijay Matheswaran

The Magnus effect is an aerodynamic phenomenon that describes the lift force generated by a rotating body due to asymmetric airflow and pressure distribution. This project explores the potential of integrating leading-edge rotating cylinders (LERCs), which induce the Magnus effect, into airfoil designs to enhance lift and stall characteristics, particularly at Short Take-Off and Landing (STOL) conditions. Computational analyses have shown that LERCs can significantly improve lift coefficients and stall angle of attack, particularly at low Reynolds numbers. These results have been verified through experimental low-speed wind tunnel testing. Experimental testing also showed improved boundary-layer attachment and reduced flow separation. Ground-effect in takeoff and landing performance studies emphasize the importance of lift augmentation, such as flap deployment, yet most research has not incorporated Magnus effect-based flow control mechanisms in operational flight at STOL conditions. To address these limitations, this project proposes an experimental approach incorporating a rotating cylinder airfoil model in wind tunnel testing. By measuring lift and drag coefficients, this experiment aims to provide further support for the Magnus effect鈥檚 applicability to practical aircraft designs, specifically focusing on its feasibility for air tractors and other STOL-reliant platforms.

Characterization of Wing Frames Under Torsional Loading

MEMBERS: Aiden Holt, Kazune Tazawa

ADVISOR: Dr. Suresh Raju

This study investigates the torsional behavior of open-frame, skeletal structures commonly found in remote-controlled aircraft. These structural configurations are popular due to their lightweight designs; however, accurately predicting their torsional stiffness is a challenge using typical methods. Traditional torsion theories used for monocoque designs are insufficient when applied to open-frame structures due to geometric discontinuities and complicated load paths. While Finite Element Analysis can provide highly detailed solutions, it tends to be a time-consuming process, making high-speed prototyping a challenge.

To address the gap in theoretical applications, this study proposes a quick mechanics-based method to predict torsional stiffness and deformations in open-frame designs. This approach aims to bridge the gap between analytical simplicity and predictability, providing a fast and reliable estimation method. This research uses Digital Image Correlation (DIC) techniques to experimentally observe and measure the kinematics of deformation of various test samples with applied torsional loading. The evaluation of test data assists in validating the proposed model and also contributing a deeper understanding of the deformation mechanisms present in open-frame structures.

By combining experimental kinematic data with a simplified mechanical analysis, this work delivers a theoretical method for understanding and predicting torsional performance in remote-controlled aircraft utilizing open-frame, skeletal designs with efficiency and accuracy. 

Drag Analysis of the Common Loon Power Stroke

MEMBERS: Alyssa Rutherford, Ella Kreger, Kellsie Juhl

ADVISOR: Dr. Vijay Matheswaran

This work analyzes a model of the Common Loon in a 3 x 4 wind tunnel. Loons are exceptional swimmers with unique adaptations that enhance their diving ability. Part of this adaptation is the Loon鈥檚 power stroke sequence, which is how they move so well through the water. They have a symmetrical stroke, meaning both feet move in sync. This stroke begins in the forwardmost position with the webbing of their feet slightly extended. Then, as they push their feet back, they fully extend this webbing to produce the most thrust. Finally, they tuck their feet back behind them after completing the stroke to minimize drag as they cruise through the water using the produced thrust. For this experiment, we tested 4 foot positions at different stations of the power stroke to determine its impact on drag. Throughout the project, we collaborated with Dr. James Paruk, a Professor at St. Joseph鈥檚 College and a Common Loon expert with 23+ years of research experience. 

Experimental Verification of a Simulated Multi Element Airfoil

MEMBERS: Catalina Blair, Kenil Patel, Riley Strandberg, Lane Sherbert

ADVISOR: Dr. Vijay Matheswaran

The Schottky-Klein prime function is a special function in complex analysis. One application of the function is fluid dynamics, specifically the fluid flow around multi-element airfoils. This is highlighted in a 2023 paper by Thomas DeLillo and Christopher Green. Utilizing a NACA4415 airfoil with three elements, the method in the paper is compared to experimental coefficients of pressure at a variety of flap deflection angles and angles of attack. This is done to see when the method is most accurate, and when it is no longer applicable.

Ground Effect Characteristics of the Supersonic Bi-Directional Flying Wing

MEMBERS: Parker Struve, Seth Newton, James Wright, Joshua Amiegbebhor-Onikolase

ADVISOR: Dr. Vijay Matheswaran

The team conducted a study of the Supersonic Bi-Directional (SBiDir) Flying Wing design created by the University of Miami. The University of Miami primarily carried out Computational Fluid Dynamics (CFD) analyses of the design in supersonic flight. This led the team to ask if the SBiDir design would be feasible in the subsonic flight regime. Since this craft is primarily designed as a supersonic transport, the only occurrences of subsonic flight the team could reasonably test are in takeoff and landing, leading to the study of ground effect becoming the primary consideration of the project. The team 3D printed the design out of PETG and carried out post-processing to remove the roughness from the skin caused by the printing. The team then used the 暗网禁区破解版 3x4 wind tunnel to test the baseline cruise performance by obtaining the Lift, Drag, and Pitching Moment Coefficients as functions of angle of attack. An artificial ground plane was then introduced to the tunnel to simulate the aircraft coming close to the ground. The team tested several different distances between the ground plane and the model at various angles of attack to again obtain the Lift, Drag, and Pitching moment coefficients. The data obtained was then plotted and compared to determine what effect the ground has on the aircraft. Specifically, the team was most concerned with how the Lift to Drag ratios would compare to determine the effect of the ground on the lift and drag forces generated in the tunnel.

Group 5 Experimental Methods Project

MEMBERS: Cole Matthews, Kylen Divelbiss, Austin Sanderson, Clayton Crockett

ADVISOR: Dr. Vijay Matheswaran

Testing the effects of a shock control bump on a diamond shaped supersonic airfoil. These effects will be compared to the original diamond airfoil without a bump. We are expecting a decrease in change in wave drag due to the pressure change caused by the shock wave.

Ideal Inlet Bump Design

MEMBERS: Isaac Thompson, Silja Fahnestock, Jordan Lower, Kelsey Thurman

ADVISOR: Dr. Vijay Matheswaran

This project is testing the effectiveness of several inlet bump designs based on pressure coefficient profiles and shock wave patterns. Mock up 2D profiles will be tested in a water table. During testing water heights will be collected at various points and pictures will be taken to determine pressure and shock wave angles throughout the test section. Using this data, pressure coefficients, Mach numbers, and shock wave patterns can be found and analyzed. 

2025 (Non-Senior Design) Graduate Projects

Comparison of Strain Energy Failure Criteria with Industry Standard Fracture Toughness

MEMBER: Adam Bodenham

ADVISOR: Dr. Charles Yang

This applied learning activity seeks to draw conclusions about two methods of calculating the failure of a cracked specimen: fracture toughness and strain energy release rate. Strain energy release rate methods are common in very brittle materials, like those used in the analysis of ice, rock, and concrete. Alloyed aluminums used in aerospace, like 7050-T651 plate, do exhibit brittle failure surfaces. Applying strain energy release rate criteria, a standard corner edge through thickness crack in an aluminum sample can therefore be compared with the industry standard fracture toughness criteria. The comparison of these two valid methods is explored in this project. An energy formulation can be developed for the sample based on the internal strain energy. The results of which are compared with those from a model using fracture toughness and stress intensity calculations. The initial flaw size will be varied and the corresponding applied stress at failure will be compared.

Effects of Test Setup Deviations on Stress-Strain Curves of Composite Compression Coupons Using FE Analysis

MEMBER: Azizbek Uktamjonov

ADVISOR: Dr. Chihdar C. Yang

This study investigates the effects test set up deviations from standard procedure (ASTM D6641), such as bolt torque mismatch, coupon preload, tabbed and unstabbed coupon types on stress-strain curves in combined load compression (CLC) tests. Finite Element analysis has been used to obtain stress-strain curves for said variations based on FE material parameters developed based on physical tests.