WebDec 1, 2024 · Previous experiences on lifting body concepts, like the Northrop HL-10 and the Boeing X-20 Dynasoar [3], [4] that were developed without adoption of sophisticated computational tools, suggested the effectiveness of delta-shaped planform bodies to be used as re-entry configurations. This is also witnessed by the increasing computational ... WebFeb 28, 2014 · The wingless lifting body aircraft studied the feasibility of maneuvering and landing an aerodynamic craft designed for reentry from space. Credits: NASA Photo A fleet of lifting bodies flown at NASA's …
Low speed longitudinal aerodynamics of a blended wing-body re-entry ...
WebThe aerofoil is then drawn up into the area of low pressure, producing lift. If the air is still, it will slowly descend. A hang-glider descends at the rate of about 1 metre per second (a slow walking pace of about 3.6 km/h). In order to not lose height, a hang-glider must find air going up as fast as the glider is descending. For example, if a ... WebDec 1, 2024 · Abstract. This paper deals with the evaluation of low-speed longitudinal aerodynamic performances of a vehicle concept with an unconventional blended wing-body aeroshape. The spacecraft is intended as a multipurpose vehicle for future International Space Station payload and/or crew servicing and support, able to perform a lifting re … stanfield outfitters
Lifting Body Spacecraft With "Staged Reentry" (1964)
WebSimilarly, for lift coefficient and the lift force, the large area of the wing allows for lower fluid flow under the wing, resulting in pressure increase under the wing (lift). Thus, at greater … WebThe aerofoil is then drawn up into the area of low pressure, producing lift. If the air is still, it will slowly descend. A hang-glider descends at the rate of about 1 metre per second (a slow walking pace of about 3.6 km/h). In … WebMay 16, 2024 · The reason why I mentioned the design of merging wings into the body is because this would allow the body to contribute to the lift as well. And thus, it would create a U-shaped lift distribution as the middle of the aircraft (body) would have the largest amount of lift, and the sides (wings) would have less. $\endgroup$ – person rejecting war