IHS ESDU Estimation of rate of climb. 92019

Description
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.
Description
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.

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Estimation of rate of climb. - 92019 - IHS ESDU
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Estimation of rate of climb.
92019
Estimation of rate of climb. 92019
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.

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.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 92019
Product Name Estimation of rate of climb.
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