TASOPT.jl
  • Home
  • Examples
    • Loading and running
    • Payload-range diagram
      • Nelder Mead
      • Gradient Based Optimization
    • Sensitivities
  • Aerodynamics
    • Geometry
    • Lift
    • Drag
    • Pitching moment
    • Atmospheric properties
  • Structures
    • Wings and tails
    • Fuselage
    • Landing gear
    • Cabin sizing
  • Propulsion systems
    • Propulsion system
    • Gas Calculations
    • Heat exchangers
    • PEM fuel cells
  • Cryogenic tanks
    • Thermal and structural models
    • Homogeneous model
  • Stability
  • Mission and sizing
    • Design and evaluation
    • TASOPT Weight Model
  • Data and I/O
    • Data structure basics
    • Data structure details
    • Loading and saving models
  • Miscellaneous
    • Original Drela docs
      • TASOPT Flowchart
    • Notes for devs
Version
  • Miscellaneous
  • Original Drela docs
  • Original Drela docs
GitHub

Original Drela docs

Obtained from Mark Drela's TASOPT site where all documents and Fortran code can be found.

  • TASOPT Technical Description
  • Simplified Viscous/Inviscid Analysis for Nearly-Axisymmetric Bodies
  • Film Cooling Flow Loss Model
  • Turbofan Sizing and Analysis with Variable cp(T)
  • Thermally-Perfect Gas Calculations
  • Balanced Field Length Calculation
  • Turbofan Weight Model from Historical Data

TASOPT Flowchart

For an attempt to make graphical sense of the aircraft-sizing workflow, see here.

« Loading and saving modelsNotes for devs »

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