Analysis of Air Transportation Systems Fundamentals of Aircraft ...

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Example Runway Design for Boeing 777-200Assume a precision approach is needed for IFR conditionsRPZ =>• W 1 = 1,000 ft.• W 2 = 1,750 ft.• L = 2,500 ft.OFA• 800 ft. width and 1,000 ft. beyond runway endRSA• 500 ft. width and 1,000 ft. beyond runway endVirginia Tech - Air Transportation Systems Laboratory 114
Example Runway Design for Boeing 777-200OFARPZRunwayRSAVirginia Tech - Air Transportation Systems Laboratory 115
Page 2 and 3:
Introductory RemarksAir vehicles ar
Page 4 and 5:
Aircraft Performance Basics(Interna
Page 6 and 7:
Basic Relationships to Uderstand th
Page 8 and 9:
Atmosphere with Constant Temperatur
Page 10 and 11:
Atmosphere with Linear Temperature
Page 12 and 13:
Atmosphere with Linear Temperature
Page 14 and 15:
International Standard AtmosphereCh
Page 16 and 17:
Important Aircraft Speed Terms to K
Page 18 and 19:
Air Compressibility EffectsA mathem
Page 20 and 21:
Example ComputationBoeing 737-300 (
Page 22 and 23:
Sample Matlab Code Used (ISAM.m)Vir
Page 24 and 25:
Plot of CAS vs. TAS (Subsonic Aircr
Page 26 and 27:
Aircraft Runway Length PerformanceE
Page 28 and 29:
Functional Forms of the ForcesThe f
Page 30 and 31:
Notes on Various Parameters1) C L a
Page 32 and 33:
Remarks About the Aircraft Accelera
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Flap Angle• Angle formed between
Page 36 and 37:
Remarks• The mass of the aircraft
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• At large flap angles (> 25 degr
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A Word on Stalling and Lift-off Spe
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These considerations are necessary
Page 44 and 45:
Integration of Acceleration Equatio
Page 46 and 47:
Aircraft Speed During Takeoff RollN
Page 48 and 49:
Takeoff Roll Distance vs. Aircraft
Page 50 and 51:
General Procedure for Runway Length
Page 52 and 53:
FAR Certification ProceduresFAR 25
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Landing Distance CaseThe landing di
Page 56 and 57:
Engine-Out Takeoff CaseDictated by
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Runway Length Procedures (AC 150/53
Page 60 and 61:
Contents of Advisory Circular 150/5
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Groupings Method AC 150/5325-4 (Fig
Page 64 and 65: Sample Calculations (FAA AC 150-532
Page 66 and 67: a) If MALW > DTW use DTW in your co
Page 68 and 69: III) Landing and Takeoff Runway Len
Page 70 and 71: I) Landing Analysisa) Estimate the
Page 72 and 73: Simple interpolation for a flap ang
Page 74 and 75: c) Compute the takeoff runway lengt
Page 76 and 77: Runway Length Analysis usingAircraf
Page 78 and 79: IAD-BGR TripIAD4,200 nmBGRVirginia
Page 80 and 81: Boeing 777-200 (GE Engines)Virginia
Page 82 and 83: Computation of Fuel WeightThis anal
Page 84 and 85: Explanation of Payload-Range Diagra
Page 86 and 87: Payload-Range Diagrams Explanations
Page 88 and 89: Sample Payload Range DiagramsPayloa
Page 90 and 91: Payload Range Diagrams (B777)Virgin
Page 92 and 93: Payload Range Diagrams (A320)Virgin
Page 94 and 95: Payload Range Dagrams (A380)Virgini
Page 96 and 97: Presentation of Runway Length Infor
Page 98 and 99: Boeing 777-200 HGW Takeoff Performa
Page 100 and 101: Landing AnalysisThis analysis is si
Page 102 and 103: Reconcile Takeoff and Landing Cases
Page 104 and 105: Other Considerations in Runway Leng
Page 106 and 107: Some Runway Design TermsThe followi
Page 108 and 109: Sketch of RPZVirginia Tech - Air Tr
Page 110 and 111: Runway Object Free Area (ROFA or OF
Page 112 and 113: OFA Dimensions (Approach Cat. C and
Page 116 and 117: Climb PerformanceMany airport and a
Page 118 and 119: Climb Performance Model Simplificat
Page 120 and 121: Final Derivation of Climb Rate Expr
Page 122 and 123: Modeling Aircraft Thrust• Thrust
Page 124 and 125: Sample Thrust Variations (PW JT9D E
Page 126 and 127: Takeoff Thrust Variations with Spee
Page 128 and 129: Variations of Cruise TSFC (PW JT9D
Page 130: Typical Rate of Climb EnvelopeItera
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