Q1
#1. If TAS is increased from 300 Kts to 400 Kts with no change in altitude, configuration, or weight, by what percentage will power required change?
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Power required
#1. If TAS is increased from 300 Kts to 400 Kts with no change in altitude, configuration, or weight, by what percentage will power required change?
#2. What is the relationship between pewer required and TAS, as an aircraft accelerates above VMD?
#3. At what % of its stalling speed must a jet aircraft fly to achieve maximum endurance for a given fuel load?