gyrocopter REVO

Hello,

I tested my 3D model with the software Flow Design de Autodesk (see the message of Jukka http://www.rotaryforum.com/forum/showthread.php?t=43878).
I do not know if the values are exact but it is interesting to compare the various configurations.



First simulation without fairing, drag coefficient 0.715




USW7E4uLfePoGcKdVHSQC7TbrM_0-kE-MUvgVFT_rQSg5aR5gjEVeYFFq3ilbBVjAFzaT3LAguH_t-BAB2abpFxmNaq2yBZgpvFUxO43da2W8BG2EvoP_Sz579WcJaQ5O2OT5QVFZWtQI5v3T4o4QFNo5hR2wqNMBv1BUcZf-mfInBMnPr6S_P45hbwjF5cRgUp8nqOGfHjVfAUvVR9FE3RSSBsYQ0o_vpHh3ApvSjr3BiflMp4mENfea3Vv1Ik6FEUO5XVOvhXrYGC6SuW2PPsYRyKBabFDmTClnu5ECZJbvCIXfH1_h12M7cTn2lbC0ZTBVDyrFigca2wjN33cvZzNAJ6LvKHa7eA0Y96z-Xz0b62PPypaGFIYGssdk_C2fmBU0DrEkZY5uOi5-AiPLFNk-rAWCvrduwqHyvSRGwWLpY7_LWctXVcPrwyOOtfN3D8OqgrXGXvF238pHpmVpOV6A-bgKQrUQH8Cpp3O6R_CoGVq3Yj4Wfr-b7e70jR39LvC_zaO0UhT5pM_CQTv3_JOT8Jdv19Njjq-B50-f_I=w1398-h758-no






The second simulation with fairing, drag coefficient 0.347




hnoOo3MEdy1W6qEZQL7fKeQ516uEZmEQIO7gQlkKuLrkXC3BEWq3UVXO3O8LjjbSviL5xLX93VvxfXWDeTljv-rrn_BzaTMnrK_lps-Ko3mc7PoD5UPUFeVJSijSZtDfhm-zKEyGY65t0-7aAYIWObhRMZEcW5Lv5d2JnUncOwub9lOA6VBBrki4QBzGvKtS17ylt6UxrcP1dgJ_kLrLGbLdzTVgQGQeTdAmj5i8arWE4sbZDlE2NXs-nRQZ-0QpNMLX9wOoDrR5f0jT323JwaD__VhUfi7oLMv8X5wpnjuMnSGVyCu7RfQWyv0ojN7t0T2hC0esEltT2PA0NIYObfizTH307CxZLld5_9RQfThcKv3wkmZqH7QOdZkS8u6FAL4N2xi5sXv1Q6Gv8BPqPEo9LN5iqpPhg4z9J81_zwlmfKQDT-lG6b1DRiZZ0zj2FsIkcrHGh7UqI2RIg8MNqHUd7gtjCKeSkK2Am8QQrEM6IqhVCbfl1wwYgHTkjkpXboxn4zXHRfdkqA2NeKmYj2l-0EPJeBXVHAJMrxyrTyk=w1398-h758-no






The third simulation with brought in landing gear, drag coefficient 0.285




Sp9C18vLnyXr2t_MxjoTLGOCZ8A8s__5TLgIiwXVKXUqQwjhNYyjJEpFugP5-QflvWLgBfwpE5KmKUBIcOMH4BpABlAg7RZpEGV0w3svEVpgkwQRg8RB7fs8G4r2Vi06ZxzKF7VFDCQzIbb1-FPlpHcjSVtgkaV2yyJQ8MXa-KSWFCC76Jmj_zD-_v69DVR_EbkeuEuDKSfgse5XJ47_gjYxiSzRRtkzqZ3M-dUglE_FUBBBo_jWQV29gajxCCjFKsoK-KISRpMuPj5k5wMsgR0T8DvH_MZmqGHWwb50O3OFK6Fk8Ez_g6m8nDiiYxTuyVFyv3T6USwOWpaUCq5ym8b0hFZzCDjr5gHzK0PO6QN0GWRytFFg5DM84e0OMAldvkJxP5ZOm6qkua_U_1ktNFmvv1VFGjvR6Zke40KJ67u1MyxNMcvyCYwK57-HyqZODYArccLpNHAVWJTCcbas14Geg8vea18uiRTw3_hUQ6zcvhhp5P_FVQoJ1TYYPt8MCQguGxOqXL1_2T92hXOH4Bc4mwqxLv7S-j0vrd_m8E4=w1398-h758-no






The fourth simulation without mast nor head of rotor, where from the interest of a fairing of mast, drag coefficient 0.249




-MJ446GFkcqcHHtJp7WD6atCqKsaDa4a-UXlLW_6cuxadRvFDmohlbFKQWKCkcwomNl4dMjLB5s5v3nhmfY_Wolxdv_XdEc4qCiJi72mBUrFeYtdT-0xQ4GOzat0qD3jGDIIwFySPJ3N0mMOzYPkTV-3cQ0dBVGSILCyf0UBTPwt-EHGQ5hQtySjchlFNAl0sfww8Q1e4V3zb6SeFWVuBsEMVxjm2c5Viy7DJUaupLzkbbQ7M_mbKUZiTkoHX5jFCJADSEV_uvloO7xYKD0uWx0SsvxyjKo92fk00z4goi49AeCIQUNYlgV4Ep0X3K1OaWXl97ybDaz4U7VzAqdW_9oUXoDktx8JCJFrBeOjpzLgiNHeM7abDyVfimcKkrxAe6cCRkTf1ewabKChz0bB7BMa-qC-AR266TqtUYF2kogPGOCZOFEy54B0k4sLLjYmJMI9M_b2Iv4VMoCIN9t30zCDZxRzovRTy-2gu66ZeThhB5Lb4x3fHoGB-iKT5VJ_jU_6dKdAyyNfxofj-XbCIGzlCBNvZVErI1BwqPPNyuM=w1398-h758-no




Panpan
 
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