Aero Fact: Why Winglets Reduce Drag
Winglets mitigate wingtip vortices and reduce induced drag, improving fuel burn.
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Winglets mitigate wingtip vortices and reduce induced drag, improving fuel burn.
The altitude at which the rate of climb drops to a specified minimum.
Staging improves mass fraction and delta-v by discarding empty hardware.
At high altitude, IAS drops while TAS and Mach diverge due to air density changes.
The lowest free-stream Mach at which local airflow first reaches sonic speed on the airframe.
Swept wings delay compressibility effects and reduce wave drag at transonic speeds.
Stall speed increases with aircraft weight due to lift coefficient and load factor.
Laminar vs. turbulent boundary layers change skin friction and separation behavior.
Isp measures thrust per unit propellant flow—higher Isp means more efficient engines.
A key performance metric for both aircraft and rockets affecting acceleration and climb.
Bank angle directly increases load factor, impacting stall speed and structural limits.
Mission planning revolves around total delta-v required including gravity and drag losses.