|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/198 ; 244/130 ; 244/200|
|§371/§102 date||19820930 (19820930)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 16 인용 특허 : 7|
A wing-mounted pod for preventing an unstable increase in the pitching moment of a swept-wing aircraft due to increasing speed and angle of attack is disclosed. This invention is for use on a swept-wing aircraft of the type having a nonlinear, unstable increase in its pitching moment due to a loss of lift at the outboard wing above a predetermined angle of attack at high Mach numbers. For an aircraft having a single, strut-mounted engine on each wing, the pod is placed along the intersection of the upper surface of the wing and the inboard side of the en...
In an aircraft of the type having a nonlinear, unstable increase in the pitching moment above a predetermined angle of attack for a predetermined aircraft speed, said aircraft having a wing with a leading edge and an upper surface, an improvement comprising: means located on said upper surface of said wing for forming a shock in the air flowing over the upper surface of said wing at said predetermined aircraft angle of attack of said wing and at an aircraft speed above a Mach number of approximately 0.6, said shock causing localized separation of the air...