Detailed Example of Aircraft Performance Calculations: Climb ...

More documents

Recommendations

Info

Definition of Terms to Estimate Engine ThrustT 0,M= Thrust at sea level and at Mach number M (Newtons)T 0,M =0= Thrust at sea level and at Mach = 0 (zero speed) (Newons)λ = Rate of change of thrust vs. Mach number (lapse rate) (Newton/Mach)M true= True mach number (dimensionless)T h,M= Thrust at altitude h and Mach number Mρ h= Air density at altitude h (kg/m 3 )ρ o= Air density at sea level (zero altitude) (kg/m 3 )m = Thrust lapse rate (dimensionless)Virginia Tech - Air Transportation Systems Laboratory12
A Simple Aircraft Model for Engine Thrust• The following picture provides a visual effect of the thrust modelThrustT0,M=0-λT0,MT 0,M= T 0,M =0− λM trueT h,M= T 0,M⎛ ρ h⎝⎜ ρ 0⎞⎠⎟mTh,MThrust line at sea levelThrust line at altitudeMach Number (Mtrue)Virginia Tech - Air Transportation Systems Laboratory13
Page 4 and 5: Example - Aircraft Climb Performanc
Page 8 and 9: Calculation Procedure• Step 1: Es
Page 10 and 11: Aircraft Climb Performance2,000 fee
Page 18 and 19: Aircraft Climb Performance8000 m (2
Page 20 and 21: Aircraft Climb Performance8000 m (2
Page 22 and 23: Rate Of Climb Analysis• Repeating
Page 24 and 25: Sensitivity AnalysisRate of Climb v
Page 26 and 27: Implications for Real-world Aviatio
Page 28 and 29: Eagle County Airport (EGE)source: F
Page 30 and 31: Departure Procedure from EGE(Runway
Page 32 and 33: Departure Procedure from EGE Airpor
Page 34 and 35: UnrestrictedClimbAnalysis.m• Main
Page 36: UnrestrictedClimbAnalysis.m• Outp

Detailed Example of Aircraft Performance Calculations: Climb ...

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?