IHS ESDU Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Rate of climb. PERF RP1/2

Description
ESDU Perf RP 1/2 gives formulae derived using the method of ESDU PERF RP 1/0 for the incremental correction of flight measured rate of climb data to temperatures and weights differing from those applying at the time of test. Two temperature correction cases are considered: one above full throttle height and one below. For the latter and for weight correction, simple formulae give the increments in rate of climb, and graphs are provided to assist in their evaluation. Above full throttle height the measured pressure height is corrected for the temperature change rather than the rate of climb. A correction for wind gradient is also provided. A worked example illustrates the use of the method.
Description
ESDU Perf RP 1/2 gives formulae derived using the method of ESDU PERF RP 1/0 for the incremental correction of flight measured rate of climb data to temperatures and weights differing from those applying at the time of test. Two temperature correction cases are considered: one above full throttle height and one below. For the latter and for weight correction, simple formulae give the increments in rate of climb, and graphs are provided to assist in their evaluation. Above full throttle height the measured pressure height is corrected for the temperature change rather than the rate of climb. A correction for wind gradient is also provided. A worked example illustrates the use of the method.

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Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers.  Rate of climb. - PERF RP1/2 - IHS ESDU
London, United Kingdom
Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Rate of climb.
PERF RP1/2
Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Rate of climb. PERF RP1/2
ESDU Perf RP 1/2 gives formulae derived using the method of ESDU PERF RP 1/0 for the incremental correction of flight measured rate of climb data to temperatures and weights differing from those applying at the time of test. Two temperature correction cases are considered: one above full throttle height and one below. For the latter and for weight correction, simple formulae give the increments in rate of climb, and graphs are provided to assist in their evaluation. Above full throttle height the measured pressure height is corrected for the temperature change rather than the rate of climb. A correction for wind gradient is also provided. A worked example illustrates the use of the method.

ESDU Perf RP 1/2 gives formulae derived using the method of ESDU PERF RP 1/0 for the incremental correction of flight measured rate of climb data to temperatures and weights differing from those applying at the time of test. Two temperature correction cases are considered: one above full throttle height and one below. For the latter and for weight correction, simple formulae give the increments in rate of climb, and graphs are provided to assist in their evaluation. Above full throttle height the measured pressure height is corrected for the temperature change rather than the rate of climb. A correction for wind gradient is also provided. A worked example illustrates the use of the method.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number PERF RP1/2
Product Name Standard British method of performance reduction for piston-engined aircraft with constant-speed propellers. Rate of climb.
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