Recent content by malay_555

as minger said you have to keep in mind the brayton cycle while designing the jet engine , but the operating parameters are depending upon your initial requirements, i.e. for which aircraft are you designing, what is the speed of it, how much force required to propel it, its altitude, which type...

hey Cyrus, every new idea of invention starts with imagination so imagineering is the best engineering, n by the way the idea of this kind of propulsive system is conceptually correct, the problem is just we don't have the proper source of antimatter.

Use of this kind of engine on Earth anti matter can be stored only in magnetic field flow control can be done by this magnetic field so no need of pump the impulse of the product of process will be very less as it is only energy there is no material, so some working fluid also be subjected to...

for aircarft design i suggest you (along with abve listed) 1) Aircraft Design Projects for engineering students - Lloyd R. Jenkinson,James F. Marchman 2) Aircaft Performance and design - J D Anderson 3) The design of the aeroplane - Darrol stinton 4) Aircraft design (i think auther is cork)...

yes the shock will generate on the uper side. you can easily find this kind of cases in any of the missile aerodynamics books as wedge shaped airfoil is used in it.

You can directly use the energy eq here upstream air energy = downstream air energy + your turbine power in wind turbines generally potential energy change is negligible so you can directly use the kinetic energy power = upstream KE - downstream KE here mass low rate(m) is also const...

i think your topic is to design a blade, 1) for that you have to first decide your operating range of the wind turbine means a speceific value of wind speed, it may be assumed or selected for perticuler location on the basis of atmospheric data, 2) then you also have to fix your rpm of turbine...