¡¡¡¡µL¶qºõ°Ñ¼Æ dimensionless parameter
µL±Û¬y irrotational flow
µLÀ£¬y free surface flow
µLÖߩʬyÊ^ nonviscous fluid, inviscid fluid
ª«²z¸Ñ physical solution
ª«²z°Ï°ì physical domain
§l¥X suction
µ}²¨ªi rarefaction wave
µ}²¨¯x°}¤À¸Ñªk split coefficient matrix method
§Æº¸¯Séw©Ê¤ÀªR Hirt stability analysis
²Óªø«× slenderness
²ÓªøÊ^ slender body
Åã®æ¦¡ explicit scheme
¬Û®e±ø¥ó consistency condition
¬Û¦ü²z½× similarity theory
¬Û¦ü«ß similarity law
¬Û¦ü©Ê¸Ñ similar solution
ÅTÀ³ÀW²v response frequency
®ø¯à energy dissipation
·¤¬y wedge flow
±×¿Eªi oblique shock wave
±×ªï·®æ¦¡ skew-upstream scheme
Á»ô¤½¦¡ Chezy formula
«¬ªý profile drag
§Îª¬¦]¤l shape factor
×¥¿·L¤À¤èµ{ modified differential equation
±ÛÁu¤ô¦À rotating arm basin
À£[¤O]° pressure drop
À£[±j¤ô]ÀY pressure head
À£®t differential pressure
À£®tªý¤O pressure drag
À£¤O¯à pressure energy
À£±j¶Ç·P¾¹ pressure transducer
À£±jp manometer
À£ÁYªi compression wave
¨ÈÁn³t¬y[°Ê] subsonic flow
·Ïµ·ªk smoke wire method
l®g diffraction
³÷¬y weir flow
¸¬]¬y cascade flow
²GÊ^°Ê¤O¼í·Æ hydrodynamic lubrication
²GÊ^°Ê¤O¾Ç hydrodynamics
²GÊ^ÀR¤O¾Ç hydrostatics
²GÊ^ÀRÀ£ hydrostatic pressure
¨Ì¿à°ì domain of dependence
ÉÝ«¬y density current, gravity flow
Ál©¶ chord
Ál«¬ airfoil
³±¼vªk shadow method
Áô®æ¦¡ implicit scheme
ªï·®æ¦¡ upstream scheme , upwind scheme
ªï¨¤ angle of attack
¼vÅT°ì domain of influence
¯Fªi surge wave
ªo½¤Åã¥Ü oil film visualization
ªo·ÏÅã¥Ü oil smoke visualization
¦³Ê^¿nªk finite volume method
¦³±Û¬y rotational flow
¦³À£¬y pressure flow
»¤¾É³t«× induced velocity
»¤¾Éªý¤O induced drag
¹w¦ô®Õ¥¿ªk predictor-corrector method
·½ source
»·³õÃä¬É±ø¥ó far field boundary condition
»·³õ¬y far field flow
¬ù§ô´õ confined vortex
¤Ãæi¬y homoentropic flow
¹B°Ê¬Û¦ü kinematic similarity
¹B°ÊÖß©Ê kinematic viscosity
¦A¼h¬y¤Æ relaminarization
¦Aªþ reattachment
¼ÈºA¬y transient flow
Ö߫״ú©wªk visco[si] metry
Öß«×p visco[si] meter
Öߩʬy[°Ê] viscous flow
§é®g refraction
®¶¿º¬y oscillatory flow
»]µo evaporation
¥¿¿Eªi normal shock wave
¤ä°t¤èµ{ governing equation
ª½½uªk method of lines
«ü¼Æ®æ¦¡ exponential scheme
½èÂIªk particle method
½èÂIÊI®æªk particle in cell method, PIC method
½è¶q¶Ç»¼ mass transfer
½è¶q¦uùÚ conservation of mass
º¢¦Z lag
º¢¤î¬y stagnation flow
«¤Oªi gravity wave
©P´Á¬y periodic flow
¶b¹ïºÙ¬y axisymmetric flow
ª`¤J injection
¾nÂI stagnation point
¾n´õ standing vortex
ª¬ºA¤èµ{ equation of state
À@§Î¬y conical flow
ã©w±`¬y quasi-steady flow
ãÃЪk pseudo-spectral method
¦Û°ÊÊI®æ¥Í¦¨ automatic grid generation
¦Û¥Ñ¹ï¬y natural convection, free convec-tion
¦Û¥Ñ¬y free stream
¦Û¥Ñ¬y½u free stream line
¦Û¥Ñ± free surface
¦Û¥Ñ®g¬y free jet
Á`À£[¤O] total pressure
Á`À£ÀY total head
Á`ÖU total enthalpy
ªý¤O drag, resistance
ªý¥§»~®t damping error
¦÷¿ñª÷ªk Galerkin method
¾Ã¤ô¦±½u back water curve
Ö`µo¹Lµ{ bursting process
ÖU«p«× enthalpy thickness
æi¨ç¼Æ entropy function
æi±ø¥ó entropy condition
æi³q¶q entropy flux
[¦Û]ÓìÀ³ÊI®æ [self-] adaptive mesh
CFL±ø¥ó Courant- Friedrichs- Lewy condition ,CFL condition
KDU¤èµ{ KDV equation
U§ÎºÞ U-tube
®J§J¯S¼Æ Eckert number
¶øº¸-¯Á¥½µá¤èµ{ Orr-Sommerfeld equation
¶ø¨¯¬y Oseen flow
¤Ú¶ë¯S¤O Basset force
ªO¶ôªk panel method
¥bÁô®æ¦¡ semi-implicit scheme
Á¡Ál²z½× thin-airfoil theory
«O³æ½Õ®t¤À®æ¦¡ monotonicity preserving diffe-rence scheme
ÃzÅF detonation
Ãz¬µ explosion
²¦¶ø-Âĥﺸ©w«ß Biot-Savart law
¾À°Å¤Á³t«× friction velocity
¾À°ÅÀ³¤O skin friction, frictional drag
¾À®ÄÀ³ wall effect