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• De Laval nozzle
  {{lowercase|title=de Laval nozzle}}{{subpages}} {{Image|De Laval nozzle 2.png|right|300px|Diagram of the gas flow through a de Laval nozzle used to produce supersonic velocity of the exhaust gases from a rocket engi
  10 KB (1,535 words) - 13:11, 23 October 2021
• De Laval nozzle/Bibliography
  759 bytes (115 words) - 01:54, 6 April 2010
• De Laval nozzle/Definition
  A de Laval nozzle is a tube, pinched in the middle, which is used to accelerate a hot, pressu
  297 bytes (51 words) - 10:26, 3 April 2010
• De Laval nozzle/Related Articles
  498 bytes (66 words) - 16:03, 3 April 2010
• De Laval nozzle/External Links
  186 bytes (26 words) - 15:02, 5 April 2010

Page text matches

• Convergent-divergent nozzle
  #REDIRECT[[De Laval nozzle]]
  28 bytes (4 words) - 10:28, 3 April 2010
• Con-di nozzle
  #Redirect[[De Laval nozzle]]
  28 bytes (4 words) - 10:30, 3 April 2010
• De Laval nozzle/Definition
  A de Laval nozzle is a tube, pinched in the middle, which is used to accelerate a hot, pressu
  297 bytes (51 words) - 10:26, 3 April 2010
• Choked flow/Related Articles
  {{r|de Laval nozzle}}
  251 bytes (32 words) - 02:40, 17 April 2010
• Rocket engine/Related Articles
  {{r|De Laval nozzle}}
  423 bytes (55 words) - 16:25, 10 February 2024
• Injector/Related Articles
  {{r|De Laval nozzle}}
  284 bytes (34 words) - 16:32, 10 February 2024
• Venturi tube/Related Articles
  {{r|De Laval nozzle}}
  557 bytes (70 words) - 13:17, 20 March 2010
• Jet engine/Related Articles
  {{r|de Laval nozzle}}
  960 bytes (122 words) - 13:07, 22 July 2012
• De Laval nozzle
  {{lowercase|title=de Laval nozzle}}{{subpages}} {{Image|De Laval nozzle 2.png|right|300px|Diagram of the gas flow through a de Laval nozzle used to produce supersonic velocity of the exhaust gases from a rocket engi
  10 KB (1,535 words) - 13:11, 23 October 2021
• Rocket engine
  ...the propellant combustion) increasing from slow (green) to fast (red) in a de Laval nozzle as used in rocket engines.}} ...elocity|velocities]]. Most usually, rocket propelling nozzles are of the [[De Laval nozzle|de Laval]] type as depicted in the adjacent Figure 1.
  16 KB (2,555 words) - 02:46, 13 March 2024
• Injector
  ...'' or '''steam injector''' is a device that uses the Venturi effect of a [[de Laval nozzle|converging-diverging nozzle]] to convert the [[pressure]] energy of a motiv
  6 KB (972 words) - 16:30, 10 February 2024
• Choked flow
  ...restriction<ref>A [[valve]], a [[convergent-divergent nozzle]] such as a [[de Laval nozzle]], an [[orifice plate]] hole, a leak in a gas pipeline or other gas contain ...tes can be used to produce a particular mass flow rate. Choked flow in a [[de Laval nozzle]] as used in a [[rocket engine]] can be accelerated to [[supersonic]] linea
  12 KB (1,845 words) - 16:31, 10 February 2024
• Jet engine
  ...y pressure/ambient pressure) is very high, it may be worthwhile to use a [[de Laval nozzle|convergent-divergent (de Laval) nozzle]] to maximize the thrust. As the nam ...hey emit it at the much higher speeds which are made possible by using a [[de Laval nozzle]] to accelerate the engine exhaust. This is why they are suitable for aircr
  63 KB (9,748 words) - 13:17, 2 February 2023