SU72141A1 - The way to combat the median effect of high-speed aircraft with swept wings - Google Patents
The way to combat the median effect of high-speed aircraft with swept wingsInfo
- Publication number
- SU72141A1 SU72141A1 SU358089A SU358089A SU72141A1 SU 72141 A1 SU72141 A1 SU 72141A1 SU 358089 A SU358089 A SU 358089A SU 358089 A SU358089 A SU 358089A SU 72141 A1 SU72141 A1 SU 72141A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- combat
- way
- speed aircraft
- median effect
- swept wings
- Prior art date
Links
Landscapes
- Testing Of Engines (AREA)
Description
Целью изобретени вл етс борьба со срединным эффектом скоростных самолетов со стреловидными крыль ми. Срединный эффект в значительной степени снособ|Ствует образованию срывов у стреловидных крыльев, увеличива их сопротивление.The aim of the invention is to combat the median effect of high-speed aircraft with swept wings. The median effect is largely due to the formation of stresses in the swept wings, increasing their resistance.
Дл борьбы со срединным эффектом в месте сочленени крыльев с фюзел жем располагаютс щелевидные отверсти с направл ющими / (фиг. 1), поставленными под углом к набегающему потоку. Через эти отверсти производитс отсос пограничного сло .In order to combat the median effect, slit-like apertures with guides / (Fig. 1) at an angle to the incident flow are located at the junction of the wings with the fuselage. The boundary layer is sucked through these holes.
Предмет изобретени Subject invention
Способ борьбы со срединным эффектом скоростных самолетов со стреловидными крыль ми, отличающийс тем, что в местах сочленени крыльев с фюзел жем расположены щелевые отверсти , через которые производитс отсос пограничного сло .The method of dealing with the middle effect of high-speed aircraft with swept wings, characterized in that in the articulations of the wings with the fuselage there are slotted holes through which the boundary layer is sucked.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU358089A SU72141A1 (en) | 1947-07-26 | 1947-07-26 | The way to combat the median effect of high-speed aircraft with swept wings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU358089A SU72141A1 (en) | 1947-07-26 | 1947-07-26 | The way to combat the median effect of high-speed aircraft with swept wings |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2081280A Addition SU514663A2 (en) | 1974-12-08 | 1974-12-08 | The method of machining with advanced plastic deformation |
Publications (1)
Publication Number | Publication Date |
---|---|
SU72141A1 true SU72141A1 (en) | 1947-11-30 |
Family
ID=48248766
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU358089A SU72141A1 (en) | 1947-07-26 | 1947-07-26 | The way to combat the median effect of high-speed aircraft with swept wings |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU72141A1 (en) |
-
1947
- 1947-07-26 SU SU358089A patent/SU72141A1/en active
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