Numerical simulation of flow past bodies by vortex method Alexey Setukha Lomonosov Moscow State...

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Numerical simulation of flow past bodies by vortex method Alexey Setukha Lomonosov Moscow State University September, 2013

Transcript of Numerical simulation of flow past bodies by vortex method Alexey Setukha Lomonosov Moscow State...

Page 1: Numerical simulation of flow past bodies by vortex method Alexey Setukha Lomonosov Moscow State University September, 2013.

Numerical simulation of flow past

bodies by vortex method

Alexey Setukha

Lomonosov Moscow State University

September, 2013

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• The idea of a vortex methods

• Mathematical aspects

• The numerical vortex model for the separated flows past bodies

• The tests calculations and examples of Applications

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NUMERICAL SCHEME

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THE PROBLEM

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The tests calculations and

examples of Applications

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MODERN PASSENGER AIRCRAFT MODELING

PERSPECTIVE VIEW

TOP VIEW

SIDE VIEW

AIRCRAFT MAPPING

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MODERN PASSENGER AIRCRAFT MODELING

For angles of attack 0 , 10

For angles of attack 40 ,50 ,60 ,70 ,80

SEPARATION LINES

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MODERN PASSENGER AIRCRAFT MODELING

VORTEX WAKE FOLLOWING AIRCRAFT WHEN 70 .

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MODERN PASSENGER AIRCRAFT MODELING

DISTRIBUTION OF AERODYNAMIC LOAD:

p

p pc

q

at solid fuselage, p

p pc

q

- at wings and fins (thin surfaces), 2 / 2q V .

70

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MODERN PASSENGER AIRCRAFT MODELING

COMPARING CALCULATIONS TO EXPERIMENTAL DATA

-0,8

0

0,8

1,6

2,4

-5 15 35 55 75

Cy

mz

-2,1

-1,4

-0,7

0

0,7

-5 15 35 55 75

NORMAL POWER AND PITCH MOMENT COEFFICIENTS ON VARIOUS ANGLES OF ATTACK

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

VELOCITY FIELD ANALYSIS

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

HOUSE MAPPING. POSITION OF BASE LINE OF PRESSURE COMPARISON.

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

THE DISTRIBUTION OF PRESSURE COEFFICIENT OVER HOUSE SURFACE

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

THE DISTRIBUTION OF PRESSURE COEFFICIENT IN SECTION A-A

(COMPARISON TO EXPERIMENT).

0 300

line-calculation, points- experiment (K.S. Strelkov, M.S. Komarov, Yu. M. Mulov, Yu.M. Nevezhina Scientific report of NTO STz “TsAGI-TEST” 1998)

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MODELING FLOWS PAST BUILDINGS AND CONSTRUCTIONS

THE DISTRIBUTION OF PRESSURE COEFFICIENT IN SECTION A-A

(COMPARISON TO EXPERIMENT).

0 300

line-calculation, points- experiment (K.S. Strelkov, M.S. Komarov, Yu. M. Mulov, Yu.M. Nevezhina Scientific report of NTO STz “TsAGI-TEST” 1998)

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MODELING PARACHUTES

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MODELING PARACHUTES

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MODELING PARACHUTES

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Parachute Building Institute (Moscow, Russia) Parachute design department (Xianfan, China)