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 wings

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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
Application number
SU358089A
Other languages
Russian (ru)
Inventor
О.А. Чембровский
Original Assignee
О.А. Чембровский
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by О.А. Чембровский filed Critical О.А. Чембровский
Priority to SU358089A priority Critical patent/SU72141A1/en
Application granted granted Critical
Publication of SU72141A1 publication Critical patent/SU72141A1/en

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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.

SU358089A 1947-07-26 1947-07-26 The way to combat the median effect of high-speed aircraft with swept wings SU72141A1 (en)

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)

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