Recent content by ravachol

i think i didn't write the problem obviously. I have to design a personal aircraft with 1600 km range and the pav must have one engine. At first glance, I chose a turboprop engine but then aero-diesel engines became more reasonable for me. If you have any opinion, I will be glad to hear

for my design project, i have to consider a feasible prop systm for a single engine propellr driven aircraft and I am thinking about diesel engines. they seem very efficient and cheap for aircraft propulsion. ill have a small number for power/ weight ratio but it will be cheaper and it wll use...

thank you , hundred times, again Astronuc.

i was exactly asking the same think that Brewnog thought; why turboprops and turbofans were used as opposed to turbojets for military cargo airplanes and thanks to all for answering.

I think my question is obvious :wink: Most of the cargo planes, almost every, use turbo props or turbofans; c 130, c 160, cn 235, a 400 m.. I am wondering that what makes props choosable for cargo planes ?

i've read sth like there cannot be a mountain higher than 15000 meters because of the gravity. this was like a do you know statements in magazines. is there anyone knows sth about that

this is the one that i am searching definitely. thanks a lot

i want to learn a second language but i need ur advice what you think about the secondary language is better in this industry. i am in trouble with german, french and spanish. german seems closer but i want to ask you, too. thanks for ur care..

i find myself the answer its true to take Cp as specific heatcoefficient if ther is flow work extra with heat exchange

do we use Cp just for processes with flow work or ther is anything more related with this, is my question thanks for ur help..

especially no, that was just a homework of definitions and some examples for a general information and the rationale of these ways thanks anyway for ur care..

1.aerodynamics 2.designing the dynamic of an air\ spacecraft that have the best performance\cost ratio 3.the most known NASA or lockheed martin and also TAI(in Turkey) 4.a good geometry and aerodynamics knowledge the rest after sorry ı have to go

i'll only answer the last part of your question in which you askedis ther any chance to work outside the industry aerospace engr'g is similar to mechanical eng as you can see easily, both have same courses but aerospace is the spezialized. thus i want to mean you can work anywher that produces...

yes and also strain hardening an maybe alloys i am reaaly in trouble and have a homework tomorrow..

is there anybody help me for learning hardening ways, links or anything else thanx