hi dantheman999 my suggestion is cfd. Have u done an analysis using it?or if u have access to windtunnel u can model it and compute the forces involving it.
theoretical solutions may give a value close to the approximate values.
thanks a lot rb1957,i am a working scientist and we have equipments and tunnel to carry out just wanted to check what else is new on this field
thanks again for ur info
cfd we have inhouse code and the results are converging
I am testing an 1:15 scaled model aircraft on an wind tunnel at M=1.6 my aim is to find effect of installed loads on Stores.Just want to know the existing methods followed.
I just want to know the difference between axisymmetric thrust vectoring nozzles and ordinary nozzles and the aerodynamics involved in axisymmetric nozzles and its benefits
Any link regarding the matter will be helpful
hello
I am an aeronautical engineer and I need datas on the effect of fins and flares on the base drag of cylindrical afterbodies. Any links on the subject will be helpful