Modern Channel-wing/VTOL Research (English ... - CAFE Foundation

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The Universal fairing and correct layout finding to carry the largest in the world <strong>wing</strong> console of An 124 and AN 225. July, 2009
The refinement of An225 Aerodynamics. July, 2009
Page 1 and 2: Information about the author July,
Page 3: Аn-72 works, Coanda effect, the wi
Page 7 and 8: The An-148 aerodynamics refinement.
Page 9 and 10: Integrated studies of Combined Wing
Page 11 and 12: the Combined Wing Aerodynamic chara
Page 13 and 14: VTOL convertible airplanes. July, 2
Page 15 and 16: STOL airplane AN-70 with the propwa
Page 17 and 18: General view of The Custer Channelw
Page 19 and 20: The Combined Wing Scheme at the cru
Page 21 and 22: The specifics of The Combined Wing
Page 23 and 24: The Combined Wing load distribution
Page 25 and 26: The Combined Wing MAC determining M
Page 27 and 28: The Combined Wing top plane with wi
Page 29 and 30: The Straight Wing Lift Force. July,
Page 31 and 32: The Straight Wing and Channel Secti
Page 33 and 34: Straight Wing drag. July, 2009
Page 35 and 36: The Combined Wing Induced Drag Calc
Page 37 and 38: The Combined Wing structural scheme
Page 39 and 40: Finite Element Analysis scheme of t
Page 41 and 42: Bending Moment Scheme for different
Page 43 and 44: The Combined Wing properties compar
Page 45 and 46: The Channel Wing Model July, 2009
Page 47 and 48: Combined Wing in cruise configurati
Page 49 and 50: Combined Wing model in AT-1 wind tu
Page 51 and 52: The Cy(α) Chart of Combined Wing,
Page 53 and 54: The Cy(α) chart of Combined Wing m
Page 55 and 56:
L/D ratio chart of the combined win
Page 57 and 58:
The Combined Wing aircraft model wi
Page 59 and 60:
The Combined Wing model with wingle
Page 61 and 62:
Aircraft model with Straight Wing,
Page 63 and 64:
The airplane model with equivalent
Page 65 and 66:
The aircraft model with Combined Wi
Page 67 and 68:
Longitudinal stability chart mz(α)
Page 69 and 70:
The Cy(α) graph of the model with
Page 71 and 72:
The Cy(α) graph of the model with
Page 73 and 74:
Cy(α) of the model with Combined W
Page 75 and 76:
The lift comparison of the same mod
Page 77 and 78:
The Experimental airplane with Comb
Page 79 and 80:
Control System. July, 2009
Page 81 and 82:
Side View. July, 2009
Page 83 and 84:
Upper View. July, 2009
Page 85 and 86:
Left View. Flap deflection δз=0.
Page 87 and 88:
The Cabin. July, 2009
Page 89 and 90:
The airplane in the year of 2009. J
Page 91 and 92:
The Layout. July, 2009
Page 93 and 94:
Mean Technical Data of the Experime
Page 95 and 96:
Experimental Research of the Produc
Page 97 and 98:
The AOA dependent Lift Coefficient
Page 99 and 100:
The AOA dependent Lift Coefficient
Page 101 and 102:
The Engine of the Experimental Airp
Page 103 and 104:
The Powerplant Testbed of 181 July,
Page 105 and 106:
The Envelope of 181 at δз=45° G0
Page 107 and 108:
The Ultralight Backpack VTOL Projec
Page 109 and 110:
The Homo Avis Project. July, 2009
Page 111 and 112:
Backpack VTOL Aircraft Trek Springt
Page 113 and 114:
Experimental VTOL aircraft XFY-1 Po
Page 115 and 116:
Backpack VTOL Aircraft with Combine
Page 117 and 118:
Projections of the Backpack VTOL Ai
Page 119 and 120:
The Flight Trajectory of BA Product
Page 121 and 122:
Модель изделия РС (
Page 123 and 124:
General view of BA parked. July, 20
Page 125 and 126:
General View of BA (Мк-2). July,
Page 127 and 128:
The Flight Envelope of BA(Мк-1) J
Page 129 and 130:
The experimental research of projec
Page 131 and 132:
Remotely controlled model of BA. Ju
Page 133 and 134:
Testing on the tied up stand. July,
Page 135 and 136:
BA model with piston engines July,
Page 137 and 138:
BA model with piston engines on the
Page 139 and 140:
Free flight model testing. July, 20
Page 141 and 142:
The BA model in the wind tunnel. Ju
Page 143 and 144:
Aerodynamics of the BA model. With
Page 145 and 146:
The proposed scheme of the passenge
Page 147 and 148:
Conclusion. July, 2009
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Modern Channel-wing/VTOL Research (English ... - CAFE Foundation

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