Estimation of rate of climb.
Abstract:ESDU 92019 presents the equations with varying degrees of simplification for the calculation of rate of climb of jet-powered or propeller-driven aeroplanes. It is primarily concerned with "steady-state climbs", that is with instantaneous climb rate, and does not treat the effect of acceleration introduced by a climb schedule. The general calculation procedure is illustrated by a worked example based on a jet-powered combat aircraft. For propeller-driven aeroplanes, approximate guidance is given graphically on maximum climb rate as a function of power/weight ratio. It is based on comparisons of computed data for a wide range of aircraft configurations, using typical propellers having a given variation of efficiency with speed, with published data for a large number of aircraft types with fixed- or variable-pitch propellers driven by piston or turbo-prop engines. Approximate guidance on the speed for best climb rate is also given, based on the computed results. A worked example shows how the data might be used at the preliminary project stage to assess maximum climb rate or, alternatively, installed power to achieve a given rate of climb.
|Data Item ESDU 92019|
- Aircraft Noise
- Fatigue - Endurance Data
- Fatigue - Fracture Mechanics
- Fluid Mechanics, Internal Flow
- Fluid Mechanics, Internal Flow (Aerospace)
- Heat Transfer
- Physical Data, Chemical Engineering
- Stress and Strength
- Transonic Aerodynamics
- Vibration and Acoustic Fatigue
- Wind Engineering
Aerospace Materials Data
Additional Engineering References