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1 nozzle-exit
nozzle-exit pressureдавление на срезе сопла -
2 nozzle exit
1) Космонавтика: выходная часть сопла, выходной срез сопла, закритическая часть сопла, расширяющаяся часть сопла2) Макаров: выходное сечение сопла, срез сопла -
3 nozzle exit
(выходной) срез сопла, выходное сечение сопла -
4 nozzle exit
выходной срез сопла; выходная часть [выход] сопла; расширяющаяся [закритическая] часть сопла -
5 nozzle exit section
Большой англо-русский и русско-английский словарь > nozzle exit section
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6 nozzle exit angle
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7 nozzle exit area
1) Авиация: выходное сечение сопла2) Космонавтика: площадь выходного сечения сопла -
8 nozzle exit cone
Авиация: выходное сопло -
9 nozzle exit diameter
Техника: диаметр выходного сечения сопла -
10 nozzle exit plane
Космонавтика: плоскость среза сопла -
11 nozzle exit pressure
1) Авиация: давление на выходе из сопла2) Военный термин: давление в выходном сечении сопла3) Техника: давление в выходном срезе сопла -
12 nozzle exit section
1) Техника: срез сопла2) Космонавтика: выходная часть сопла, выходное сечение сопла -
13 nozzle-exit conditions
Универсальный англо-русский словарь > nozzle-exit conditions
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14 nozzle-exit plane
Космонавтика: плоскость выходного сечения сопла -
15 nozzle-exit pressure
1) Авиация: давление на срезе сопла2) Космонавтика: давление на выходе из сопла -
16 nozzle exit area
Англо-русский словарь по гражданской авиации > nozzle exit area
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17 nozzle-exit pressure
Англо-русский словарь по гражданской авиации > nozzle-exit pressure
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18 nozzle exit area
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19 nozzle exit pressure
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20 nozzle-exit pressure
См. также в других словарях:
de Laval nozzle — Diagram of a de Laval nozzle, showing approximate flow velocity (v), together with the effect on temperature (t) and pressure (p) A de Laval nozzle (or convergent divergent nozzle, CD nozzle or con di nozzle) is a tube that is pinched in the… … Wikipedia
De Laval nozzle — A de Laval nozzle (or convergent divergent nozzle, CD nozzle or con di nozzle) is a tube that is pinched in the middle, making an hourglass shape. It is used as a means of accelerating the flow of a gas passing through it to a supersonic speed.… … Wikipedia
Propelling nozzle — A propelling nozzle is a component of a jet engine that is found at the tail of the engine that operates to form an exhaust jet and to maximise the use of the exhaust gas s energy throughout the engine so that the maximum overall thrust is… … Wikipedia
Bell nozzle — The Bell shaped or Contour nozzle is probably the most commonly used shaped nozzle. It has a high angle expansion section ( 20 to 50 degrees) right behind the nozzle throat; this is followed by a gradual reversal of nozzle contour slope so that… … Wikipedia
propelling nozzle — A convergent/divergent duct in the exhaust system of a gas turbine engine, where the remaining gas energy is converted into velocity to produce thrust. In a gas turbine engine, the exit velocity of gases is subsonic at low thrust conditions only … Aviation dictionary
fixed-area nozzle/fixed-area exhaust nozzle — On a jet engine, an exhaust nozzle exit opening that remains constant in the area. See exhaust nozzle … Aviation dictionary
Rocket engine nozzle — A rocket engine nozzle is a propelling nozzle usually of the de Laval type used in a rocket engine to expand and accelerate the combustion gases, from burning propellants, so that the exhaust gases exit the nozzle at hypersonic… … Wikipedia
Expanding nozzle — The expanding nozzle is a type of rocket nozzle that, unlike traditional designs, maintains its efficiency at a wide range of altitudes. It is a member of the class of altitude compensating nozzles, a class that also includes the plug nozzle and… … Wikipedia
Plug nozzle — The plug nozzle is a type of rocket engine nozzle that, unlike traditional designs, maintains its efficiency at a wide range of altitudes. It is a member of the class of altitude compensating nozzles, but unlike the aerospike, the plug design is… … Wikipedia
Altitude compensating nozzle — An altitude compensating nozzle is a class of rocket engine nozzles that are designed to operate efficiently across a wide range of altitudes.Conventional designsThe basic concept of any engine bell is to efficiently direct the flow of exhaust… … Wikipedia
pre-exit thrust reverser — A thrust reverser system installed forward of the exhaust nozzle. See thrust reverser … Aviation dictionary