SAE Technical Paper Series 1977
DOI: 10.4271/770470
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Flight Test Evaluation of a Method to Determine the Level Flight Performance of a Propeller-Driven Aircraft

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“…The most common approach is to determine aircraft drag using data from power-off glides. Then Ẇu is determined from the equality of thrust and drag in steady flight and P mech is determined either by direct measurement of engine torque or from calibrated engine performance curves (Bridges 1976). Another approach is to determine drag from the change in aircraft performance after a known, incremental increase in drag and then compute η P as before (Bridges 1976).…”
Section: Introductionmentioning
confidence: 99%
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“…The most common approach is to determine aircraft drag using data from power-off glides. Then Ẇu is determined from the equality of thrust and drag in steady flight and P mech is determined either by direct measurement of engine torque or from calibrated engine performance curves (Bridges 1976). Another approach is to determine drag from the change in aircraft performance after a known, incremental increase in drag and then compute η P as before (Bridges 1976).…”
Section: Introductionmentioning
confidence: 99%
“…Then Ẇu is determined from the equality of thrust and drag in steady flight and P mech is determined either by direct measurement of engine torque or from calibrated engine performance curves (Bridges 1976). Another approach is to determine drag from the change in aircraft performance after a known, incremental increase in drag and then compute η P as before (Bridges 1976). In this case, it is not necessary to assume equality of aircraft drag in powered and unpowered flight.…”
Section: Introductionmentioning
confidence: 99%