A keen understanding of nozzle design principles and experience with relevant software tools is essential. If you have a passion for aerospace engineering and can deliver high-quality work, we would love to hear from you. It would be good to have a background using ansys ...
nozzleballoon flightThis paper describes a unique project developed by a group of students at the Department of Mechanical Engineering of Louisiana State University with a focus on the design, building, and testing of a rocket nozzle system on a high-altitude student platform (HASP). HASP ...
rendering, and collaborative CAD modeling functions in Fusion 360. He has worked closely with his fellow student team members, including Rodrigo Yurazcek (nozzle design and CFD simulations), Manuela Becerra (engine propellant chemicals), and Isabella Crespo and Osheit Chang (coding and flight simula...
Software Offerings AxSTREAM: Integrated CAE Platform for Supersonic and Hypersonic Technology Thermal Fluid System Design: Rocket Engine Layout – Cycle Calculation Nozzle Design & Cooling Turbopump Secondary Flow Systems Propellant Pipelines Generative Turbomachinery Design & Analysis: ...
Nozzles tend to be either two- or three-dimensional. Heat transfer characteristics, particularly in the throat, where the peak heat flux occurs, are not well understood. Heat transfer predictions for these small thrusters have been made with one-dimensional analysis such as the Bartz equation or...
For ideal nozzles, basically two different types of shock structures in the plume may appear for overexpanded flow conditions, a regular shock reflection or a Mach reflection at the nozzle centreline. Especially for rocket propulsion, other nozzle types
• Detailed design of turbine and pump components • Secondary flow systems and force analysis • Rotor dynamics and bearing analysis • Nozzle sizing and cooling Who Should Attend: We are encouraging engineers, designers, project managers, and other technical professionals working in start-ups...
Shock pattern in the plume of rocket nozzles: needs for design consideration Hagemann,G.,Frey,... - SHOCK WAVES -BERLIN- 被引量: 28发表: 2008年 Shock pattern in the plume of rocket nozzles: needs for design consideration Hagemann, G., Frey, M.: Shock pattern in the plume of rocket ...
BurnSim is a solid rocket steady-state internal ballistics simulation software package for the Windows platform. A rocket motor simulator. Solid propellant grain design. In a nutshell, input your motor, nozzle and propellant characteristics and BurnSim calculates the Kn through the burn and predicts...
A Computer-Aided Design (CAD) system for solid rocket motor nozzle based on microcomputer is described.The developed software can accomplish a series of structure designs and performance calculations by way of man-machine interaction.At last,a number of data files,charts and engineering drawings will...