A method for calculating a fuel consumption differential corresponding to an aircraft changing from an original trajectory (which incorporates the cost model of the airline through speed and altitude parameters within the flight plan) to a revised trajectory, the method including (1) calculating a ...
Fuel consumption per passenger per kilometre is calculated according to the operating data of all aircraft in the Cathay fleets. Taking aircraft types on individual flights into account would significantly complicate the calcula...
Lastly, if your airplane has an airspeed indicator equipped with a true airspeed ring, you can input altitude and temperature and read true airspeed on your airspeed indicator. Know your Pilot Operating Handbook and become familiar with the information available for your aircraft.” (NEW) IFR Mast...
Use of stagnation temperature in calculating rate of heat transfer in aircraft heat exchangers No Abstract Available GP Wood - 《Technical Report Archive & Image Library》 被引量: 4发表: 1943年 Research on the Inversion of Equivalent Surface Heat Transfer Coefficient of Mass Concrete by Calculating...
A method for calculating a fuel consumption differential corresponding to an aircraft changing from an original trajectory (which incorporates the cost model of the airline through speed and altitude parameters within the flight plan) to a revised trajectory, the method including (1) calculating a ...
Fuel consumption per passenger per kilometre is calculated according to the operating data of all aircraft in the Cathay fleets. Taking aircraft types on individual flights into account would significantly complicate the calculat...
One method estimates the vertical flight speed and fuel consumption of an aircraft at a point along a flight plan by using other aircraft parameters for that point. The process uses a database having entries comprising sets of actual values of operating parameters acquired during previous flights ...
Some examples are given, together with estimates of steam consumption. A suggestion is also given for reducing the turbo-pump weight.Saunders, D. JRoyal Aircraft Establishment