Incompressible Turbulent Boundary Layer Flow Over a Yawed Flat Plate |
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Page 1
... chordwise direction are independent of the spanwise flow ( references 2 and 3 ) . Hence the chordwise flow can be calculated with no ref- erence to the spanwise flow and the results then used This will be defined to calculate the ...
... chordwise direction are independent of the spanwise flow ( references 2 and 3 ) . Hence the chordwise flow can be calculated with no ref- erence to the spanwise flow and the results then used This will be defined to calculate the ...
Page 21
... chordwise . flow . For the yawed plate then , t = 250,000 ( cos 30 ) = 216,000 is determined by and by a sandpaper width of 1 in .; and should be taken in the chordwise direction . Experiments were carried out on the unyawed plate to ...
... chordwise . flow . For the yawed plate then , t = 250,000 ( cos 30 ) = 216,000 is determined by and by a sandpaper width of 1 in .; and should be taken in the chordwise direction . Experiments were carried out on the unyawed plate to ...
Page 26
... chordwise direction ( see equation III - 12 ) & 2 = { ( R , N ) = RYKS бо kx T / s kx Ris -16 COS Λ ( IV - 9 ) while for the unyawed plate , S - S ( R , 0 ) = kx = ( IV - 10 ) R / 5 If the thickness is measured at a fixed chordwise position ...
... chordwise direction ( see equation III - 12 ) & 2 = { ( R , N ) = RYKS бо kx T / s kx Ris -16 COS Λ ( IV - 9 ) while for the unyawed plate , S - S ( R , 0 ) = kx = ( IV - 10 ) R / 5 If the thickness is measured at a fixed chordwise position ...
Common terms and phrases
६० Assume the virtual Booth's results boundary layer equations boundary layer growth boundary layer thickness calculate chordwise direction chordwise flow continuity equation determined dimensional displacement thickness downstream Equations II-1 EXPERIMENTAL POINTS experimental results experiments Figure 18 Figure 22 flow goes straight flow quantities free stream velocity function g goes straight back growth law Hence INCHES independence principle laminar flow leading edge lift coefficients mean velocity component momentum thickness MYCY NACA pitot tube PLATE YAWED 30 POCIELA pressure distribution rake Reynolds number sandpaper width shape parameter shearing stress shown in Figure simple sweep theory spanwise flow stagnation point streamwise direction STREAMWISE DISTANCE streamwise flow streamwise growth strip of sandpaper swept thickened Traversing Mechanism turbulent boundary layer turbulent flow turbulent layers two-dimensional unswept wing unyawed plate virtual origin wall yawed and unyawed yawed flat plate yawed plate YAWED WINGS yawhead Young and Booth ар бх لا