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Gen. Thomas P. Stafford Looks At The Display In The Hallway At Stafford Elementary, Weatherford Daily News 2022 Southwestern Oklahoma State University

Gen. Thomas P. Stafford Looks At The Display In The Hallway At Stafford Elementary, Weatherford Daily News

Articles

Gen. Thomas P. Stafford looks at the display in the hallway at Stafford Elementary, which is named in his honor. His two sons, Stas, right, and Michael look on.


Gen. Thomas P. Stafford Elementary School And Weatherford Stafford Airport Terminal Dedications November 21 & 22, 2022, Weatherford Daily News 2022 Southwestern Oklahoma State University

Gen. Thomas P. Stafford Elementary School And Weatherford Stafford Airport Terminal Dedications November 21 & 22, 2022, Weatherford Daily News

Articles

A collection of photos from the dedications of Stafford Elementary and Stafford Airport Terminal, seen in the November 23rd, 2022 issue of the Weatherford Daily News.


Weatherford Stafford Airport Celebrates New Terminal, Weatherford Daily News 2022 Southwestern Oklahoma State University

Weatherford Stafford Airport Celebrates New Terminal, Weatherford Daily News

Articles

The City of Weatherford and Oklahoma Aeronautics Commission will host a special public celebration and ribbon cutting of the new Weatherford Stafford Airport Terminal.


New Schools Personal For Project Manager, Weatherford Daily News 2022 Southwestern Oklahoma State University

New Schools Personal For Project Manager, Weatherford Daily News

Articles

Gen. Thomas P. Stafford Elementary started construction in 2020, having a hand in building Stafford Elementary and East Intermediate was personal for Project Manager Shawn Bonner.


Stafford Highlights - Famed Astronaut Returns For 40th Anniversary Of Apollo Mission, Weatherford Daily News 2022 Southwestern Oklahoma State University

Stafford Highlights - Famed Astronaut Returns For 40th Anniversary Of Apollo Mission, Weatherford Daily News

Articles

Above, Lt. Gen. Thomas P. Stafford speaks during the anniversary event in Weatherford December 7, 2012, of Apollo 17.

At top right, Michael, Thomas and Stas Stafford are pictured with Cosmonaut Valery Kubasov during the 40th Anniversary of Apollo 17 December 7, 2012.


Astronaut Snoopy’S 50-Plus Year History With Nasa, Weatherford Daily News 2022 Southwestern Oklahoma State University

Astronaut Snoopy’S 50-Plus Year History With Nasa, Weatherford Daily News

Articles

"Unknown to many, Snoopy has been working with NASA since the late 1950s"


Local Astronaut May Command U.S.-Russian Flight (Reprint From 1972), Weatherford Daily News 2022 Southwestern Oklahoma State University

Local Astronaut May Command U.S.-Russian Flight (Reprint From 1972), Weatherford Daily News

Articles

EDITOR’S NOTE: this story first appeared in the November 2, 1972, edition of the Weatherford Daily News, 50 years ago today, about Lt. Gen. Thomas P. Stafford’s chance to commence a U.S.-Russian space flight.


Mitigation Of The Laminar Separation Bubble Using Active Vortex Generators, Hayden Hitt 2022 University of Alabama in Huntsville

Mitigation Of The Laminar Separation Bubble Using Active Vortex Generators, Hayden Hitt

Summer Community of Scholars Posters (RCEU and HCR Combined Programs)

No abstract provided.


Experiments To Mitigate Flow Recirculation In A Closed Anechoic Chamber Using Mesh Screens As Turbulence Suppressors, Tori Kay Wolverton 2022 Mississippi State University

Experiments To Mitigate Flow Recirculation In A Closed Anechoic Chamber Using Mesh Screens As Turbulence Suppressors, Tori Kay Wolverton

Theses and Dissertations

The desire to gather acoustic data of a propeller in simulated hover without environmental effects is met with the challenge of recirculating flow in a closed anechoic chamber. Flow recirculation in an anechoic chamber is not ideal because the effects of it being ingested by the rotor cause unsteady loadings on the propeller. This unsteady loading causes vortex noise from the turbulence introduced by the recirculation of the flow. The aim is to study the acoustic signature of a propeller separate from external factors and engine noise. Two different propellers with three different screen combinations were tested in a closed ...


Foundations For Finite-State Modelling Of A Two-Dimensional Airfoil That Reverses Direction, Jake Michael Oscar Welsh 2022 Washington University in St. Louis

Foundations For Finite-State Modelling Of A Two-Dimensional Airfoil That Reverses Direction, Jake Michael Oscar Welsh

McKelvey School of Engineering Theses & Dissertations

Current 3-D finite-state wake models are incapable of simulating a maneuver in which the sign of the free-stream velocity changes direction and the rotor enters its own wake -- as might occur in the case of a helicopter which ascends and then descends. It is the purpose of this work to create a 2-D finite-state wake model which is capable of handling changes in free-stream direction as a precursor to development of a 3-D model that can do the same.

The 2-D finite-state model used for reentry modifications is an existing model created by Peters, Johnson, and Karunamoorthy. By the addition ...


Design And Analysis Of Aircraft Wing, prabhat dixit Graduate Engineer, Vivek Rathod Graduate Engineer, Deshmukh Chetan Pravin Graduate Engineer, Piyush Patil Graduate Engineer 2022 Department of Aerospace Engineering, SOET, Sandip University, Nashik, Maharastra, INDIA

Design And Analysis Of Aircraft Wing, Prabhat Dixit Graduate Engineer, Vivek Rathod Graduate Engineer, Deshmukh Chetan Pravin Graduate Engineer, Piyush Patil Graduate Engineer

Graduate Research in Engineering and Technology (GRET)

This research develops and analyses a general aviation plane. A preliminary representation of the eventual product is used to start the design process for an airplane. Based on a drawing, a design mission profile is utilized to determine the weight. A more advanced approach is used to estimate weight, which employs calculated performance criteria to produce a more exact weight estimate. The wing design has been demonstrated to be a feasible alternative for a similar general aviation aircraft. When traveling through air or other fluids, a wing is a type of fin that provides lift. Airfoils may be observed on ...


Experimental And Computational Investigation Of Divergent Thrust Losses In Rocket Nozzles, Vaibhav Arya Graduate Engineer, Anushka Sunil Kapse Post Graduate Student 2022 Sandip University, MH, INDIA

Experimental And Computational Investigation Of Divergent Thrust Losses In Rocket Nozzles, Vaibhav Arya Graduate Engineer, Anushka Sunil Kapse Post Graduate Student

Graduate Research in Engineering and Technology (GRET)

The nozzle is a critical component of any rocket engine because it transforms high pressure and high temperature (with sluggish net velocity) within the combustion chamber into high velocity but low pressure. Individually, the molecules in the mixed propellants have rapid velocity in the combustion chamber, but directions are randomly pointing in all directions. A convergent-divergent nozzle, also known as a CD nozzle, is fashioned like a tube with two bulging ends and a thin part in the center. This structure/design provides the nozzle with a balanced shape. By turning the flow's heat energy into kinetic energy, the ...


A Study On Concepts De-Laval Nozzle Using Cfd Tool, Krishna Yadav Graduate Engineer, Digambar Daware Mr., Vedant Akolkar, Pallavi Padalwar 2022 Department of Aerospace Engineering Sandip University

A Study On Concepts De-Laval Nozzle Using Cfd Tool, Krishna Yadav Graduate Engineer, Digambar Daware Mr., Vedant Akolkar, Pallavi Padalwar

Graduate Research in Engineering and Technology (GRET)

A device that is used to control the characteristics of fluid is known as a nozzle. Its primary function is to increase the fluid's rate of motion. A traditional De-Laval nozzle will have three distinct parts: a throat, a converging section, and a diverging part. This paper will attempt to detail the bulk of the nozzle concepts developed by De Laval. This paper provides a comprehensive analysis of the nozzle's operational philosophy. In addition, theoretical flow analysis is carried out at a number of locations along the length of the nozzle. The dynamic changes in flow parameters such ...


Hybrid Rocket Propulsion Development And Application, AKSHAY GHARAT Assistant Professor, VINAYAK HASTAK Graduate Engineer 2022 SOET, Sandip University, MH, INDIA

Hybrid Rocket Propulsion Development And Application, Akshay Gharat Assistant Professor, Vinayak Hastak Graduate Engineer

Graduate Research in Engineering and Technology (GRET)

Satellite technology is advancing. Satellite propulsion requires several desired rocket properties. This is necessary for 1 kg of payload. Launch vehicles no longer need rocket engines. Application includes satellite movement, orbit transfer, and probe and lander propulsion. Space travel is inventive and exciting.

Research, production, and use costs must be decreased to make space transportation systems generally available. Security shouldn't be affected. Rocket propellants must be high-performing, non-toxic, and safe. Rocket engines have other parts. Restarting and throttling are crucial. These are inaccessible to solid rocket motors. Developing a liquid rocket engine is hard and expensive, but it can ...


Engine Performance On Atomization Of Fuel Injector: A Review, Ankit Patil Er., Akshay C. Bedke Er., Vedant A. Deshmukh Er., Pratiksha Y. Shevare Er. 2022 Department of Aerospace Engineering, SOET, Sandip University, Nashik, INDIA

Engine Performance On Atomization Of Fuel Injector: A Review, Ankit Patil Er., Akshay C. Bedke Er., Vedant A. Deshmukh Er., Pratiksha Y. Shevare Er.

Graduate Research in Engineering and Technology (GRET)

The impact of the fuel injection of fuel atoms on engine performance has been investigated to improve fuel efficiency and waste disposal features. The fuel swirl method for injection atomization was evaluated both by the analysis of the fuel flow and the sample test. The goal of the paper is to establish good fuel atomization over the range of engine performance. As a result of our studies, it has been concluded that the desired atomization can be achieved when gasoline is thrown into a circular motion. Fuel spray and atomization features play an important role in the performance of internal ...


Aerospace Components Made By Polymer Material, Minal Babar Graduate Engineer, Priyansh Saxena Graduate Engineer, Nilesh Vilash Thube Graduate Engineer, GOKUL RAJ S Engineering Graduate 2022 Department of Aerospace Engineering, Sandip University, MH, INDIA

Aerospace Components Made By Polymer Material, Minal Babar Graduate Engineer, Priyansh Saxena Graduate Engineer, Nilesh Vilash Thube Graduate Engineer, Gokul Raj S Engineering Graduate

Graduate Research in Engineering and Technology (GRET)

The aerospace and aviation industry have fasted growing industries on a global scale. Reliable aircraft demands many top rubber components. These rubber components must-have high performance and endurance properties, since they will be exposed to a range of extreme weather conditions, such as excessively hot or cold temperatures, and different types of oils and gases. Rubber products are becoming more famous because of their durability under extreme environmental conditions and cost-effectiveness. The rubber used for aircraft must be of high quality, and this factor is most important in the production of the necessary parts. To study the effect of all ...


Manufacturing Process And Emerging Advantage Of Graphene Based Composites In Aerospace- A Review, Vaibhav Arya Graduate Engineer, Arjun N Prof. 2022 Sandip University, MH, INDIA

Manufacturing Process And Emerging Advantage Of Graphene Based Composites In Aerospace- A Review, Vaibhav Arya Graduate Engineer, Arjun N Prof.

Graduate Research in Engineering and Technology (GRET)

The cardinal pillar for this paper is to showcase the composition of Graphene-based composites and reveal the hidden uses of Graphene-based composites in aerospace dominion. This paper briefly discusses the different methods by which graphene-based composites can be synthesized mostly those with functional polymers and inorganic nanostructures and additionally covers a few of the applications of graphene-based composites such as lightweight, fire retardancy, and additive manufacturing. Moreover, this detailed paper also brings up crucial highlights where graphene-based composites have covered long distances from the research lab to commercialization, specifically focusing on aerospace industries.


Editorial, Shiva Prasad U Mr., M. Suresh Kumar Prof.(Dr.) 2022 Sr. Asst. Professor Department of Aerospace Engineering, Sandip University, SOET, NASHIK, MH

Editorial, Shiva Prasad U Mr., M. Suresh Kumar Prof.(Dr.)

Graduate Research in Engineering and Technology (GRET)

This special edition is devoted to Rockets and Missile Technology, a developing sector that will likely increase significantly as rocket and missile design technology progress. Modern military arsenals must contain advanced guided-weapons technology. As the need for missile and rocket technology grows, they are employed in various applications. Technological advancements additionally highlight the system's capabilities, functions, and applications, improving its efficacy and use. When it comes to combat aircraft, the armaments that go with them decide the price. New technology and applications such as hypersonic weaponry, long-range rockets and missiles, and space-based military equipment produce market upheaval. Current rocket ...


Structural Loads And Preliminary Structural Design For A World Speed Record-Breaking Turbo-Prop Racing Airplane, Matthew G. Slymen 2022 California Polytechnic State University, San Luis Obispo

Structural Loads And Preliminary Structural Design For A World Speed Record-Breaking Turbo-Prop Racing Airplane, Matthew G. Slymen

Master's Theses

The Cal Poly SLO Turbo-Prop Racer project aims to design a world speed record-breaking aircraft, capable of flying more than 550 miles per hour on a 3-kilometer closed course. To further this endeavor, this thesis presents the calculations of load distributions across the aircraft’s wing and tail and preliminary structural estimates of primary structural components for verification of the loads calculations and for use in a future finite element model. The aircraft’s fundamental design characteristics effect on the structure of the aircraft, namely the unique Y-tail design, are first examined. Then, loads are calculated in accordance with the ...


Methodology To Aircraft Design – Market Study & Design Optimization, Shreyash Attarkar, Dhananjay Ahire, Tanishq Pawar, Suresh Kumar M Prof. 2022 SOET, Sandip University, Nashik, Maharashtra, INDIA

Methodology To Aircraft Design – Market Study & Design Optimization, Shreyash Attarkar, Dhananjay Ahire, Tanishq Pawar, Suresh Kumar M Prof.

Graduate Research in Engineering and Technology (GRET)

In the last few years Aircraft have grown to be large-scale products with an increasing number of complicated systems, components, parts, and capabilities. Every single one of them. Various fields and technologies are included. Multiple sets of tools, procedures and methods are also included, as a result, to fully define, design, and develop an aircraft A comprehensive and methodic approach is required. Aircraft design that serves as a pillar in the evolution of the life cycle A balanced system solution that satisfies the needs of the customer. To accompany these characteristics. system engineering provides an interdisciplinary organization but is still ...


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