Re: 전익기용 익형

"최대두께까 두꺼운 전익기용 에어포일은 없습니까?" 아주 아주 많습니다. 그중에서 적합한 것을 고르는 것이 오히려 큰일이죠.   <IMG class=c alt="이미지를 클릭하면 원본을 보실 수 있습니다." src="https://t1.daumcdn.net/cafefile/pds8/15_cafe_2007_05_24_12_55_46550cbc58fa6" border=0> MH45는 두께가 9.85% 입니다. 모형 전익기로 아주 유명한 재기익형은 Zagi 10 (10%), Zagi 12 (12%) 입니다.   전익기 모형에서는 주로 8% 에서 12% 까지 사용합니다. 아래의 자료 참고하세요. 에어포일을 클릭하면 자세한 설명이 링크되어 있습니다.   설명을 잘 읽어보면 익하중(또는 비행속도) 이나 후퇴각에 또는 비행성격에 따라 적합한 익형을 찾아낼수 있을 겁니다.   Airfoils for...  FlyingWings   <LI><A href="http://www.mh-aerotools.de/airfoils/mh60koo.htm">MH 60</A>, t/c = 10.08% <LI><A href="http://www.mh-aerotools.de/airfoils/mh61koo.htm">MH 61</A>, t/c = 10.28% <LI><A href="http://www.mh-aerotools.de/airfoils/mh62koo.htm">MH 62</A>, t/c = 9.30% <LI><A href="http://www.mh-aerotools.de/airfoils/mh64koo.htm">MH 64</A>, t/c = 8.61% </LI>   <LI><A href="http://www.mh-aerotools.de/airfoils/mh44koo.htm">MH 44</A>, t/c = 9.66% <LI><A href="http://www.mh-aerotools.de/airfoils/mh45koo.htm">MH 45</A>, t/c = 9.85% <LI><A href="http://www.mh-aerotools.de/airfoils/mh46koo.htm">MH 46</A>, t/c = 11.39% <LI><A href="http://www.mh-aerotools.de/airfoils/mh49koo.htm">MH 49</A>, t/c = 10.50% </LI>   링크 <A href="http://www.mh-aerotools.de/airfoils/foil_flyingwings.htm">http://www.mh-aerotools.de/airfoils/foil_flyingwings.htm</A>   Airfoil Database Tailless and Flying Wings <A name=top></A> <TABLE width=625 border=0 name="Profile"> <TBODY> <TR> <TD width=140 height=8>Airfoils</TD> <TD width=50 height=8> <DIV align=center>f [%]</DIV></TD> <TD width=50 height=8> <DIV align=center>d [%]</DIV></TD> <TD width=70 height=8> <DIV align=center>cm_0</DIV></TD> <TD width=55 height=8> <DIV align=center>a_0</DIV></TD> <TD height=8>Occupation</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#mh32">MH32</A></TD> <TD width=45>2.37</TD> <TD width=45>8.71</TD> <TD width=65>-0.0580</TD> <TD width=55>-2.37°</TD> <TD>C-Wing</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#mh45">MH45</A></TD> <TD width=45>1.65</TD> <TD width=45>9.85</TD> <TD width=65>+0.0070</TD> <TD width=55>-0.27°</TD> <TD>F3B, F3F, Slope Soaring</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#mh45_8">MH45-8%</A></TD> <TD width=45>1.65</TD> <TD width=45>8.00</TD> <TD width=65>+0.0070</TD> <TD width=55>-0.27°</TD> <TD>Do not use! </TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#mh60">MH60</A></TD> <TD width=45>1.76</TD> <TD width=45>10.08</TD> <TD width=65>+0.0030</TD> <TD width=55>-0.31°</TD> <TD>F3B, F3F, Slope</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#mh60_12">MH60-12%</A></TD> <TD width=45>1.76</TD> <TD width=45>12.00</TD> <TD width=65>+0.0030</TD> <TD width=55>-0.31°</TD> <TD>Open class, Combat</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#rs004">RS 004</A></TD> <TD width=45>1.64</TD> <TD width=45>9.00</TD> <TD width=65>-0.0416</TD> <TD width=55>-1.87°</TD> <TD>F3B, Allround </TD></TR> <TR> <TD width=140 height=20><A href="http://www.aerodesign.de/english/profile/profile_s.htm#tl54">TL54</A></TD> <TD width=45 height=20>2.41</TD> <TD width=45 height=20>9.99</TD> <TD width=65 height=20>-0.0171</TD> <TD width=55 height=20>-1.20 °</TD> <TD height=20>F3B, F3F, F5B</TD></TR> <TR> <TD width=140 height=18><A>TL55</A></TD> <TD width=45 height=18>1.90</TD> <TD width=45 height=18>9.44</TD> <TD width=65 height=18>-0.0052</TD> <TD width=55 height=18>-0.68 °</TD> <TD height=18>F3B, F3F</TD></TR> <TR> <TD width=140 height=20><A href="http://www.aerodesign.de/english/profile/profile_s.htm#tl56">TL56</A></TD> <TD width=45 height=20>1.40</TD> <TD width=45 height=20>8.96</TD> <TD width=65 height=20>+0.0072</TD> <TD width=55 height=20>-0.144</TD> <TD height=20>Aerobatics, Turbine, EDF</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#sd7003">SD7003</A></TD> <TD width=45>1.46</TD> <TD width=45>8.51</TD> <TD width=65>-0.0430</TD> <TD width=55>-1.76°</TD> <TD>Thermal Soaring, Allround</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#s5010">S5010</A></TD> <TD width=45>2.20</TD> <TD width=45>9.83</TD> <TD width=65>+0.0080</TD> <TD width=55>-0.52°</TD> <TD>F3B, F3F, F5B, Allround</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#s5010_8">S5010-8%</A></TD> <TD width=45>2.20</TD> <TD width=45>8.00</TD> <TD width=65>+0.0080</TD> <TD width=55>-0.52°</TD> <TD>F3B, F3F, F5B, Slope</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#s5020">S5020</A></TD> <TD width=45>2.62</TD> <TD width=45>8.40</TD> <TD width=65>+0.0080</TD> <TD width=55>-0.70°</TD> <TD>F5B, F3B, Allround</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#s5020_8">S5020-8%</A></TD> <TD width=45>2.62</TD> <TD width=45>8.00</TD> <TD width=65>+0.0080</TD> <TD width=55>-0.70°</TD> <TD>F5B, F3B, Allround</TD></TR> <TR> <TD width=140 height=20><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs520">HS 520</A> <IMG height=14 hspace=5 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.aerodesign.de%2Ficon%2Fnew.gif" width=35 align=absMiddle></TD> <TD width=45 height=20>2.13</TD> <TD width=45 height=20>8.82</TD> <TD width=65 height=20>+0.0041</TD> <TD width=55 height=20>-0.64 °</TD> <TD height=20>F5D, F3F</TD></TR> <TR> <TD width=140 height=20><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs522">HS 522</A> <IMG height=14 hspace=5 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.aerodesign.de%2Ficon%2Fnew.gif" width=35 align=absMiddle></TD> <TD width=45 height=20>2.01</TD> <TD width=45 height=20>8.67</TD> <TD width=65 height=20>-0,0050</TD> <TD width=55 height=20>-0.84 °</TD> <TD height=20>F5D, F5B, F3F?</TD></TR> <TR> <TD width=140 height=20><A href="http://www.aerodesign.de/english/profile/profile_s.htm#eh1509">EH 1.5/9</A></TD> <TD width=45 height=20>1.50</TD> <TD width=45 height=20>9.00</TD> <TD width=65 height=20>+0.0000</TD> <TD width=55 height=20>-0.51 °</TD> <TD height=20>Aerobatics, Turbine, EDF Ex: F3B</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#eh2010">EH 2.0/10.0</A></TD> <TD width=45>2.00</TD> <TD width=45>10.07</TD> <TD width=65>+0.0000</TD> <TD width=55>-0.68°</TD> <TD>Ex: F3B, Open Class</TD></TR> <TR> <TD width=140 height=12><A href="http://www.aerodesign.de/english/profile/profile_s.htm#sipkill">Sipkill 1.7/10</A> </TD> <TD width=45 height=12>1.70</TD> <TD width=45 height=12>9.93</TD> <TD width=65 height=12>-0.0060</TD> <TD width=55 height=12>-0.76°</TD> <TD height=12>EPP Combat (Zagi)</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs3080">HS3.0/8.0</A></TD> <TD width=45>3.00</TD> <TD width=45>8.00</TD> <TD width=65>-0.0060</TD> <TD width=55>-1.20°</TD> <TD>HLG</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs3090">HS3.0/9.0</A></TD> <TD width=45>3.00</TD> <TD width=45>9.00</TD> <TD width=65>-0.0060</TD> <TD width=55>-1.21°</TD> <TD>Ex: Allround</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs3412">HS3.4/12.0</A></TD> <TD width=45>3.50</TD> <TD width=45>12.00</TD> <TD width=65>-0.0010</TD> <TD width=55>-1.25°</TD> <TD>Open Class </TD></TR></TBODY></TABLE> <TABLE width=625 border=0 name="Profile"> <TBODY> <TR> <TD width=140 height=22>Airfoils Planks</TD> <TD width=49 height=22> <DIV align=center>f [%]</DIV></TD> <TD width=50 height=22> <DIV align=center>d [%]</DIV></TD> <TD width=63 height=22> <DIV align=center>cm_0</DIV></TD> <TD width=55 height=22> <DIV align=center>a_0</DIV></TD> <TD height=22>Occupation</TD></TR> <TR> <TD height=10><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs130">HS 130</A> <IMG height=14 hspace=5 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.aerodesign.de%2Ficon%2Fnew.gif" width=35 align=absMiddle></TD> <TD height=10>1,678</TD> <TD height=10>9,652</TD> <TD height=10>+0,0157</TD> <TD height=10>-0,09°</TD> <TD height=10>Slope Soaring, DS</TD></TR> <TR> <TD height=10><A href="http://www.aerodesign.de/english/profile/profile_s.htm#jwl065">JWL-065</A> <IMG height=14 hspace=5 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.aerodesign.de%2Ficon%2Fnew.gif" width=35 align=absMiddle></TD> <TD height=10>1,687</TD> <TD height=10>7,96</TD> <TD height=10>+0,0298</TD> <TD height=10>+0,30°</TD> <TD height=10>Allround, Slope Soaring</TD></TR> <TR> <TD width=140 height=10><A href="http://www.aerodesign.de/english/profile/profile_s.htm#cj5">CJ-5</A></TD> <TD width=50 height=10>2.33</TD> <TD width=50 height=10>9.30</TD> <TD width=65 height=10>+0.0200</TD> <TD width=55 height=10>-0.10°</TD> <TD height=10>Ex: Plank, Thermal Soaring</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#cj3309">CJ-3309</A></TD> <TD width=49>3.34</TD> <TD width=50>9.41</TD> <TD width=70>+0.0190</TD> <TD width=55>-0.58°</TD> <TD>Thermik</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#cj2509">CJ-25²09</A></TD> <TD width=49>2.50</TD> <TD width=50>9.50</TD> <TD width=63>+0.0270</TD> <TD width=55>-0.13°</TD> <TD>Ex: Plank, Thermal Soaring</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#emx07">EMX-07</A></TD> <TD width=49>2.54</TD> <TD width=50>9.91</TD> <TD width=63>+0.0210</TD> <TD width=55>-0.30°</TD> <TD>Plank. F3B</TD></TR> <TR> <TD width=140><A href="http://www.aerodesign.de/english/profile/profile_s.htm#phoenix">Phönix</A></TD> <TD width=49>2.78</TD> <TD width=50>8.20</TD> <TD width=63>+0.0090</TD> <TD width=55>-0.69°</TD> <TD>Plank, F3B</TD></TR> <TR> <TD width=140 height=2><A href="http://www.aerodesign.de/english/profile/profile_s.htm#hs2080">HS 2.0/8.0</A> </TD> <TD width=49 height=2>2.00</TD> <TD width=50 height=2>8.00</TD> <TD width=63 height=2>+0.0120</TD> <TD width=55 height=2>-0.33°</TD> <TD height=2>Plank, Slope </TD></TR></TBODY></TABLE>   링크 <A href="http://www.aerodesign.de/english/profile/profile_s.htm#mh60_12">http://www.aerodesign.de/english/profile/profile_s.htm#mh60_12</A>