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Results are presented for a three surface aircraft which highlights low drag possibilities with positive static margins, presents the trade-offs between induced and profile drag, and provides insight into the aerodynamics of multiple lifting surface configurations.
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An approach, applicable to multiple-lifting-surface fixed-wing aircraft operating at subcritical Mach numbers, is presented for minimizing induced and profile drag with a constraint on the pitching moment.
Let D ∗ be the projection of the lifting surface onto the O ∗ x ∗ y ∗ plane.
The vortex theory principle is derived from the lifting line and lifting surface theories, which have been developed for airplane wings to determine wing loads and wake geometry.
For providing multiple lifting levels for a carried payload, the developed machine is equipped with a linear actuator.
Lockheed's X-33 design, besides having lifting surfaces, features a new engine called an aerospike.
Wings had already been studied extensively as the obvious lifting surfaces.
The paper presents a method for generating a time domain formulation of the lift reduction memory effect for lifting surfaces.
A five-slot contoured nozzle burner was used to create multiple lifted partially premixed flames in close proximity.
Lifting surfaces are not hydrodynamically and acoustically homogeneous and need not be acoustically compact.
Pumps that lift surface water and move it to a nearby treatment plant are called low-lift pumps.
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