Usefulness of boundary layer control (BLC) at knee of trailing edge flap, over wing nose close to leading edge or at knee of leading edge flap is shown; various methods of providing BLC are outlined, comprising slot blowing, slot suction, area suction, inclined air jets, and specially designed airfoil shapes; aerodynamic aspects of slot blowing over trailing edge flaps and wing nose are examined, and slot and area suction considered; associated practical design features required for good performance are discussed and some flight handling implications mentioned. (See also AGARD -- Report 414 Jan 1963 69 p)
Aerodynamic aspects of boundary layer control for high lift at low speeds
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 67 , n 628
1963
23 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Aerodynamic aspects of boundary layer control for high lift at low speeds
Engineering Index Backfile | 1963
|British Library Conference Proceedings | 2018
|Distributed Suction Boundary Layer Control for High Lift
SAE Technical Papers | 1968
|Distributed suction boundary layer control for high lift
Engineering Index Backfile | 1968
|Aerodynamic Problems of high lift
TIBKAT | 1962
|