RU96116559A - PLANE - Google Patents

PLANE

Info

Publication number
RU96116559A
RU96116559A RU96116559/28A RU96116559A RU96116559A RU 96116559 A RU96116559 A RU 96116559A RU 96116559/28 A RU96116559/28 A RU 96116559/28A RU 96116559 A RU96116559 A RU 96116559A RU 96116559 A RU96116559 A RU 96116559A
Authority
RU
Russia
Prior art keywords
wings
wing
mechanization
chord
combination
Prior art date
Application number
RU96116559/28A
Other languages
Russian (ru)
Other versions
RU2102287C1 (en
Inventor
А.А. Белосвет
С.А. Плясунков
Л.И. Бондаренко
А.А. Ефимов
А.Н. Давиденко
М.К. Курьянский
Original Assignee
Московское авиационное производственное объединение "МИГ"
Filing date
Publication date
Application filed by Московское авиационное производственное объединение "МИГ" filed Critical Московское авиационное производственное объединение "МИГ"
Priority to RU96116559A priority Critical patent/RU2102287C1/en
Priority claimed from RU96116559A external-priority patent/RU2102287C1/en
Application granted granted Critical
Publication of RU96116559A publication Critical patent/RU96116559A/en
Publication of RU2102287C1 publication Critical patent/RU2102287C1/en

Links

Claims (1)

Самолет, содержащий крыло со взлетно-посадочной механизацией и оперение, отличающийся тем, что крыло выполнено в виде комбинации из двух крыльев, одно из которых установлено впереди, другое позади центра тяжести самолета так, что аэродинамический фокус изолированной комбинации крыльев, находящийся от передней кромки переднего крыла на расстоянии
Figure 00000001

совпадает с центром тяжести самолета, а соотношение площадей взлетно-посадочной механизации крыльев равна
Figure 00000002

где b1 - хорда переднего крыла;
S1, S2 - хорда переднего и заднего крыла;
Figure 00000003
хорда крыла с выпущенной механизацией переднего и заднего крыла;
Figure 00000004
площадь механизации - площадь закрылка с обслуживаемой впереди него площадью переднего и заднего крыла;
Figure 00000005
производные коэффициентов подъемной силы переднего и заднего крыла;
L - аэродинамическое плечо комбинации крыльев - расстояние между линиями 25% хорд переднего и заднего крыла;
K - коэффициент торможения потока.An airplane comprising a wing with take-off and landing mechanization and plumage, characterized in that the wing is made in the form of a combination of two wings, one of which is installed in front, the other behind the center of gravity of the aircraft so that the aerodynamic focus of the isolated combination of wings is located from the leading edge of the front wings in the distance
Figure 00000001

coincides with the center of gravity of the aircraft, and the ratio of the areas of take-off and landing mechanization of the wings is
Figure 00000002

where b 1 - the chord of the front wing;
S 1 , S 2 - the chord of the front and rear wings;
Figure 00000003
wing chord with front and rear wing mechanization released;
Figure 00000004
mechanization area - flap area with the front and rear wing area served in front of it;
Figure 00000005
derivatives of the lift coefficients of the front and rear wings;
L - aerodynamic shoulder of the combination of wings - the distance between the lines of 25% of the chords of the front and rear wings;
K is the drag coefficient of the flow.
RU96116559A 1996-08-13 1996-08-13 Aircraft RU2102287C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96116559A RU2102287C1 (en) 1996-08-13 1996-08-13 Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96116559A RU2102287C1 (en) 1996-08-13 1996-08-13 Aircraft

Publications (2)

Publication Number Publication Date
RU96116559A true RU96116559A (en) 1998-01-20
RU2102287C1 RU2102287C1 (en) 1998-01-20

Family

ID=20184517

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96116559A RU2102287C1 (en) 1996-08-13 1996-08-13 Aircraft

Country Status (1)

Country Link
RU (1) RU2102287C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009004239A1 (en) 2009-01-05 2010-07-08 Ivan Novikov-Kopp Method for the complex increase of aerodynamic and transport properties, ground effect vehicle for carrying out the method (variants) and flight method

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