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Page title matches

  • '''Characteristic Exhaust Velocity''' ''V<SUB>e</SUB>'' is effective exhaust velocity and ''C<SUB>F</SUB>'' is
    957 B (123 words) - 17:00, 7 April 2007
  • '''Effective Exhaust Velocity''' </dt><BR/>A fictitious [[Exhaust Velocity|exhaust
    1 KB (194 words) - 17:00, 7 April 2007
  • '''Exhaust Deflecting Ring''' permit it to be rotated into the exhaust stream.
    567 B (78 words) - 17:00, 7 April 2007
  • '''Exhaust Stream'''
    897 B (107 words) - 17:00, 7 April 2007
  • '''Exhaust Trail''' trail]] that forms when the water vapor of an aircraft exhaust is mixed with
    875 B (113 words) - 17:00, 7 April 2007
  • '''Exhaust Velocity''' </dt><BR/>The velocity of gaseous or other particles (exhaust stream) that exhaust
    886 B (105 words) - 17:00, 7 April 2007
  • '''Fixed Area Exhaust Nozzle''' ''</dt><BR/>''On a jet engine, an exhaust nozzle exit opening which remains constant in
    699 B (87 words) - 17:00, 7 April 2007
  • #REDIRECT: [[Characteristic Exhaust Velocity]]
    46 B (4 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Effective Exhaust Velocity]]
    41 B (4 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Trail]]
    28 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Deflecting Ring]]
    38 B (4 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Stream]]
    29 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Trail]]
    28 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Velocity]]
    31 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • '''Ideal Exhaust Velocity''' </dt><BR/>The exhaust velocity of an [[Ideal Rocket|ideal
    468 B (58 words) - 17:00, 30 April 2007
  • '''Variable Area Exhaust Nozzle''' engine]], an exhaust [[Nozzle|nozzle]] of which
    880 B (111 words) - 17:00, 30 April 2007
  • #REDIRECT: [[Ideal Exhaust Velocity]]
    37 B (4 words) - 17:00, 1 May 2007
  • #REDIRECT: [[Variable Area Exhaust Nozzle]]
    43 B (5 words) - 17:00, 1 May 2007
  • #REDIRECT: [[Variable Area Exhaust Nozzle]]
    43 B (5 words) - 17:00, 1 May 2007
  • #REDIRECT: [[Variable Area Exhaust Nozzle]]
    43 B (5 words) - 17:00, 1 May 2007
  • #REDIRECT: [[Variable Area Exhaust Nozzle]]
    43 B (5 words) - 17:00, 1 May 2007
  • #REDIRECT: [[Variable Area Exhaust Nozzle]]
    43 B (5 words) - 17:00, 1 May 2007

Page text matches

  • They are relatively rare and of short duration compared to [[Exhaust Trails|exhaust trails]]''.
    846 B (109 words) - 17:00, 30 March 2007
  • is made for exchanging fresh air for exhaust-laden air during
    877 B (111 words) - 17:00, 30 March 2007
  • exhaust gases from an aircraft
    814 B (97 words) - 17:00, 30 March 2007
  • upward and divert it from the exhaust port. (d) A plate in the forward section
    1 KB (187 words) - 23:00, 30 March 2007
  • <BR/>A device used to divert the exhaust of a [[Rocket|rocket]] fired
    489 B (63 words) - 23:00, 30 March 2007
  • engine]] which receives exhaust gases separately from each cylinder,
    853 B (99 words) - 23:00, 30 March 2007
  • '''Characteristic Exhaust Velocity''' ''V<SUB>e</SUB>'' is effective exhaust velocity and ''C<SUB>F</SUB>'' is
    957 B (123 words) - 17:00, 7 April 2007
  • (''symbol c*'') = [[Characteristic Exhaust Velocity|characteristic exhaust velocity]].
    482 B (54 words) - 17:00, 7 April 2007
  • engine; and the engine-exhaust, or exhaust-moisture, type, formed by the
    1 KB (153 words) - 17:00, 7 April 2007
  • vertical position, to deflect the exhaust gases to the sides; (c) any of several different devices used on jet engines to reverse or divert the exhaust
    1 KB (181 words) - 17:00, 7 April 2007
  • often visible in a [[Rocket|rocket]] exhaust
    586 B (76 words) - 17:00, 7 April 2007
  • '''Effective Exhaust Velocity''' </dt><BR/>A fictitious [[Exhaust Velocity|exhaust
    1 KB (194 words) - 17:00, 7 April 2007
  • '''Exhaust Deflecting Ring''' permit it to be rotated into the exhaust stream.
    567 B (78 words) - 17:00, 7 April 2007
  • '''Exhaust Stream'''
    897 B (107 words) - 17:00, 7 April 2007
  • '''Exhaust Trail''' trail]] that forms when the water vapor of an aircraft exhaust is mixed with
    875 B (113 words) - 17:00, 7 April 2007
  • '''Exhaust Velocity''' </dt><BR/>The velocity of gaseous or other particles (exhaust stream) that exhaust
    886 B (105 words) - 17:00, 7 April 2007
  • '''Fixed Area Exhaust Nozzle''' ''</dt><BR/>''On a jet engine, an exhaust nozzle exit opening which remains constant in
    699 B (87 words) - 17:00, 7 April 2007
  • produced in the rocket exhaust. [[/a>|/a>
    545 B (69 words) - 17:00, 7 April 2007
  • the line of the exhaust stream. During thrust buildup and the beginning of the ''</dd><BR/>''2. In a captive test, an elbow in the exhaust conduit or [[Flame Bucket|flame
    2 KB (260 words) - 17:00, 7 April 2007
  • chambers]], a turbine, and an exhaust outlet. [[/a>|/a>
    945 B (119 words) - 17:00, 7 April 2007
  • nozzle exit area and the difference between the exhaust pressure and ambient
    1 KB (153 words) - 17:00, 7 April 2007
  • #REDIRECT: [[Characteristic Exhaust Velocity]]
    46 B (4 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Effective Exhaust Velocity]]
    41 B (4 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Trail]]
    28 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Deflecting Ring]]
    38 B (4 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Stream]]
    29 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Trail]]
    28 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Exhaust Velocity]]
    31 B (3 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • #REDIRECT: [[Fixed Area Exhaust Nozzle]]
    40 B (5 words) - 17:00, 8 April 2007
  • '''Ideal Exhaust Velocity''' </dt><BR/>The exhaust velocity of an [[Ideal Rocket|ideal
    468 B (58 words) - 17:00, 30 April 2007
  • directed velocity of all exhaust gases, a uniform gas velocity across every
    1 KB (155 words) - 17:00, 30 April 2007
  • energy]] in the exhaust jet, expressed as a ratio. [[/a>|/a>
    930 B (113 words) - 17:00, 30 April 2007
  • exhaust nozzle on a jet or rocket engine. See [[Rocket Nozzle|rocket
    684 B (87 words) - 17:00, 30 April 2007
  • isentropic expansion to ambient pressure, and exhaust at constant pressure.
    1 KB (123 words) - 17:00, 30 April 2007
  • </dt><BR/>In rocketry, the product of the cross-sectional area of the exhaust [[Jet|jet]] leaving the [[Nozzle Exit|nozzle exit]] and the difference between the exhaust pressure and the [[Ambient Pressure|ambient
    736 B (92 words) - 17:00, 30 April 2007
  • and ''c ''is the effective exhaust velocity with respect to the vehicle.
    1 KB (133 words) - 17:00, 30 April 2007
  • ...gh a [[Diffuser|diffuser]] and is mixed with [[Fuel|fuel]] and burned, the exhaust gases issuing in a [[Jet|jet]] from the rear opening. The ramjet engine can
    1 KB (168 words) - 17:00, 30 April 2007
  • ...ors]] consisting only of a [[Combustion Chamber|combustion chamber]] and [[exhaust]] [[nozzle]] to engines of some complexity incorporating, in addition, fuel
    2 KB (209 words) - 17:42, 31 January 2009
  • </dt><BR/>The exhaust [[Nozzle|nozzle]] of a [[Rocket|rocket]].
    454 B (56 words) - 17:00, 30 April 2007
  • exhaust jet, although they often contain other components, as grids, liners,
    891 B (110 words) - 17:00, 30 April 2007
  • </dd><BR/>''Specific impulse is also equivalent to the effective exhaust velocity
    1 KB (147 words) - 17:00, 30 April 2007
  • exhaust stream through changing the size and shape of the [[Throat|throat]] of the
    647 B (86 words) - 17:00, 30 April 2007
  • ...''F = mv ''where ''m ''is [[propellant]] [[mass]] [[flow]] and ''v ''is [[exhaust]] [[velocity]] relative to the [[vehicle]]. Also called ''momentum thrust.
    877 B (115 words) - 17:37, 31 January 2009
  • direction of exhaust gases so as to give additional thrust.
    1 KB (156 words) - 17:00, 30 April 2007
  • '''Variable Area Exhaust Nozzle''' engine]], an exhaust [[Nozzle|nozzle]] of which
    880 B (111 words) - 17:00, 30 April 2007
  • #REDIRECT: [[Ideal Exhaust Velocity]]
    37 B (4 words) - 17:00, 1 May 2007

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