air breathing propulsion project
$30-250 USD
Pagado a la entrega
You are to determine model the specific thrust, thrust specific fuel consumption, and overall efficiency for a range of compressor pressure ratios (0.01 to 20) and fuel to air flow ratios for ideal Scimitar [login to view URL] plots in the results section need to include specific thrust [N/(kg/s)] and thrust specific fuel consumption [kg/hr/N] vs compressor pressure ratio at fixed Mach number (M = 2 3 4 5 6) at 100,000 ft
Nº del proyecto: #12116087
Sobre el proyecto
11 freelancers están ofertando un promedio de $182 por este trabajo
Hello I am Rajesh having a PhD in aerospace engineering from a top university and fully understands your problem. I will use Matlab to do analysis and simulations. I am using Matlab for over 15 years. Please provide d Más
Hi, I am an Aerospace engineer. I have very strong analytical and problem solving skills. My priorities are quality of work and customer satisfaction. Please feel free to discuss the details of the work. Looking fo Más
Hello! I'm a postgraduate aerospace engineer (MSc degree). I'm experienced in MATLAB an Rocket propulsive systems. If you were interested to make a deal with me, Lemme know more about your project.
Hello. Will be glad to do your work. I have a big experience in engineerung, aerodynamics, programming
Hi please come for discussion. I can easily work with Matlab, SIMULINK, Inventor etc. Thanks, Scriptdesk
I have done this type of calculations many times. I can ensure that correct results are delivered and design requirements are met.