吸收
发表于 2025-3-21 19:41:50
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希望
发表于 2025-3-21 22:14:18
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使激动
发表于 2025-3-22 00:53:19
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Progesterone
发表于 2025-3-22 05:23:40
The Centrifugal (Radial) Compressor,or, which compresses the fluid intermittently in separate portions, or the rotary compressor of vane or screw or other type which compresses continuously in portions separated by moving walls or boundaries.
BANAL
发表于 2025-3-22 10:43:02
Combustion,haust gas. Some engines have a second combustion system which either reheats the flow for the later turbine stages (section 3.6.2), or burns more fuel in an afterburner behind the turbines to provide the high exhaust velocity required for the propulsion of supersonic aircraft (section C.6).
Barter
发表于 2025-3-22 13:38:33
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Barter
发表于 2025-3-22 20:06:53
,Besondere Arten von Arbeitsverhältnissen,e and temperature of the gas to fall from turbine inlet to outlet, and necessitates the use of an increasing passage area (normal to the flow) to restrain the flow to a constant velocity. This increasing area is the flare (F), shown with other typical turbine features in figure 8.1.
成份
发表于 2025-3-23 00:42:20
The Axial Flow Turbine,e and temperature of the gas to fall from turbine inlet to outlet, and necessitates the use of an increasing passage area (normal to the flow) to restrain the flow to a constant velocity. This increasing area is the flare (F), shown with other typical turbine features in figure 8.1.
Limited
发表于 2025-3-23 02:48:40
Cycle Calculations: Design Point Performance, it may make allowance for component inefficiences, pressure losses, non-ideal behaviour of gases and numerous other effects. All these affect the performance at the design point; that is, the normal operating condition of a plant or the cruise condition of an aircraft engine.
诱惑
发表于 2025-3-23 09:17:30
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