- Page 1 and 2: Information about the author July,
- Page 3 and 4: Аn-72 works, Coanda effect, the wi
- Page 5 and 6: The refinement of An225 Aerodynamic
- 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: The specifics of The Combined Wing
- 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