Aeronautical Engineering/Certain airflow conditions for aerodynamic bodies
Please, can you tell me what the airflow conditions (such as temperature, pressure, velocity and density) are for a flying aerodynamic body in front of the leading edge and near the trailing edge.
I'm guessing here you are meaning the "freestream conditions"... typically we use STP (standard temperature and pressure) at sea level unless a particular problem states otherwise...
You can google standard temperature and pressure to get the precise numbers... the velocity is the flight speed
Now you could be meaning closer to the body... under that scenario you'll need to use some sort of flow analysis to determine the flow conditions in those areas...