iCLEAN â Loitering Attack UCAV - aero.com

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PERFORMANCE CALCULATIONSMany and varied performance calculations have been made for the newand improved configuration:Thrust Calculation Results:PropertyResultMaximum thrustTmax 28[ lbf ] 902.7[poundal ]Minimum thrustTmin 14.7[ lbf ] 473.6[ poundal ]Thrust for cruise flightT 15[ lbf ] 489.5[ poundal ] 53.5% T maxVelocity Calculation Results:PropertyResultMinimum velocity (stall) - height of 0ftand 5000ft.Maximal velocity ft Vstall70.6 41.8[ knot]height0sec ft Vstall78.9 46.7[ knot]hight5000ft secVmax 110[ knots]16
Climb & Turn Calculation Results:PropertyResultMaximum climb angleMaximum dive angle climbmaxdivemax0.49[ rad] 28.2 0.51[ rad] 29.2Minimum turn radius withoutclimbing (n=4)Rmaxturn 50[ ft]Turn radius at n=2.5Rn2.5 84.6[ ft]Range and Endurance Calculation Results:PropertyResultMaximum range for climbMaximum endurance for climbMinimum range for cruiseMaximum endurance for cruiseRclimb 10.6[ NM ]Eclimb10 minRcruise 371[ NM ]Ecruise 4.6hr17
Page 1 and 2: iCLEAN - Loitering Attack UCAV1
Page 5 and 6: MARKET SURVEYMARKET SURVEY - CONFIG
Page 8: PRELIMINARY DESIGNWORK PROCESSDivid
Page 12 and 13: After beginning with the first solu
Page 14 and 15: MOMENT VS. TIME FOR DIFFERENT BOOST
Page 18 and 19: WING DETAILED DESIGNWING ROOT JOINT
Page 21 and 22: Modeling of the wing-pivot connecti
Page 23 and 24: ANALYSIS SIMULATIONA stress analysi
Page 25 and 26: WING'S FOLDING MECHANISMThe opening
Page 27 and 28: TensionDragTension forces that appl
Page 29 and 30: FINAL CONFIGURATIONAs demonstrated
Page 31 and 32: WEIGHTS TABLEThe table below descri
Page 33 and 34: THE FULL ASSEMBLY OF THE MODELAs it
Page 35 and 36: The different configurations:OPENED
Page 37 and 38: The canard's lift coefficient isn't
Page 39 and 40: CONTROL SYSTEMSIMULINK MODELWe have
Page 41 and 42: [deg]RESULTSBy entering the coeffic
Page 43 and 44: u[ft/sec]0.02Project 086755 - 02997

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