Designed for man carrying paragliders,
but can also be used in kites of the Flexifoil™ type,
see also MH 91, MH 92,
MH 93.
The openings in a parasail should be located close to the region of high
pressure around the stagnation point. This point moves in the first 5 % of the
chord length when the angle of attack covers a range from 5° to 15°. Any further
angle of attack increase makes the stagnation point move faster towards the
center of the airfoil.
The airfoils MH 91 and MH 93 show nearly the same variation. At zero lift, the
stagnation point moves to the leading edge.
x y 1.00000000 0.00000000 0.99895413 -0.00001989 0.99582360 -0.00004170 0.99063131 0.00000851 0.98341647 0.00019600 0.97423306 0.00057861 0.96314837 0.00120600 0.95024150 0.00211899 0.93560159 0.00334896 0.91932615 0.00491763 0.90151916 0.00683700 0.88228951 0.00910964 0.86174927 0.01172910 0.84001240 0.01468071 0.81719335 0.01794226 0.79340612 0.02148509 0.76876328 0.02527495 0.74337536 0.02927312 0.71735028 0.03343733 0.69079296 0.03772281 0.66380512 0.04208310 0.63648511 0.04647098 0.60892783 0.05083915 0.58122480 0.05514094 0.55346417 0.05933088 0.52573086 0.06336518 0.49810666 0.06720219 0.47067034 0.07080269 0.44349786 0.07413021 0.41666242 0.07715110 0.39023474 0.07983493 0.36428300 0.08215409 0.33887318 0.08408446 0.31406903 0.08560439 0.28993235 0.08669575 0.26652301 0.08734188 0.24389933 0.08752948 0.22211827 0.08724351 0.20123591 0.08647111 0.18130684 0.08517638 0.16232608 0.08332347 0.14428462 0.08095132 0.12723281 0.07809885 0.11121442 0.07476629 0.09624664 0.07095433 0.08233264 0.06667013 0.06944446 0.06193761 0.05756062 0.05684409 0.04672112 0.05147781 0.03697187 0.04590112 0.02837955 0.04015377 0.02096408 0.03421548 0.01466276 0.02811852 0.00944050 0.02197798 0.00531700 0.01591256 0.00232021 0.01003931 0.00052257 0.00449053 0.00001191 -0.00064095 0.00088588 -0.00511256 0.00366304 -0.00904739 0.00847543 -0.01292075 0.01494994 -0.01683908 0.02297245 -0.02076374 0.03246776 -0.02466320 0.04337799 -0.02850852 0.05564910 -0.03227394 0.06922965 -0.03593504 0.08406683 -0.03946858 0.10010697 -0.04285210 0.11729382 -0.04606256 0.13556918 -0.04907724 0.15487273 -0.05186559 0.17516161 -0.05439764 0.19639271 -0.05666848 0.21849984 -0.05867883 0.24140910 -0.06041657 0.26504493 -0.06186647 0.28933331 -0.06298886 0.31425553 -0.06375080 0.33978299 -0.06419332 0.36582666 -0.06435183 0.39229741 -0.06423615 0.41910520 -0.06385441 0.44615906 -0.06320859 0.47336707 -0.06229245 0.50065609 -0.06108806 0.52797635 -0.05960251 0.55525706 -0.05787255 0.58240229 -0.05592438 0.60931595 -0.05377096 0.63590197 -0.05141679 0.66207223 -0.04885328 0.68775996 -0.04606389 0.71292833 -0.04304751 0.73754230 -0.03983934 0.76154613 -0.03648701 0.78487704 -0.03303675 0.80746841 -0.02953777 0.82924940 -0.02604098 0.85014468 -0.02259896 0.87007400 -0.01926420 0.88895203 -0.01608794 0.90668826 -0.01311822 0.92318706 -0.01039656 0.93835391 -0.00795504 0.95209746 -0.00582509 0.96431752 -0.00403627 0.97490609 -0.00260228 0.98375779 -0.00151810 0.99077396 -0.00076206 0.99586623 -0.00029556 0.99896059 -0.00006466 1.00000000 0.00000000
Last modification of this page: 21.05.18
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