The landing-gear WERs typically used for manned |
Category: Aerospace Calculator
This category helps you to calculate the aerospace numerical like design parameters, forces, engine efficiency, etc., – WINGS OF AERO
Nacelles are structures that house the propulsion system. Nacelles can be |
Power-to-weight ratio is a measurement of actual performance of any engine or power source. It is also used as a measurement of performance of a vehicle as a whole, with the engine’s power output being divided by the weight (or mass) of the vehicle, to give a metric that is independent of the vehicle’s size.
For a horizontal tail or canard, the pitching moments which must be countered are most directly related to the wing mean chord (Cw). This leads to the “horizontal tail volume coefficient,
If the leading edge and trailing edge are parallel, the chord of the wing is constant along the wing’s length. … The average length of the chord is known as the mean aerodynamic chord (MAC).