World of Aerospace
Subsonic,
Supersonic, Transonic, Compressible, Incompressible Aerodynamics Softwares
Information and Resources
Aerodynamics Softwares
These Softwares
are used for Subsonic, Supersonic, Transonic, Hypersonic flow regimes
and Compressible and Incompressible Flow. These Aerodynamics Softwares
are used in Aerospace Engineering and Design applications
JavaFoil is a
subsonic airfoil design and analysis software that finds out a panel
method solution and is able to carry out a boundary layer calculation.
TSFoil2 is a
transonic airfoil analysis program made by NASA Ames and is able to
solve the transonic small disturbance equation using the finite
difference methods.
Pablo is a
Subsonic Airfoil Design and Analysis software that stands for "Potential
Airflow around Boundary layers coupled oneway" is a Matlab program for
airfoil design and analysis.
MS Aximer
Aerodynamics
MS Aximer free
Aerodynamics program is able to ,

Continuity
Equation (Incompressible Flow and Compressible Flow)

Bernoulli's Equation

Calculate
Pressure at Exit of Convergent Duct

Isentropic Flow Calculation

Calculate
Velocity at Throat and Exit and Area at Throat and Exit (Supersonic
Wind Tunnel)

Calculate
Airflow Velocity at the test section (Subsonic Wind Tunnel)

Calculate True
Velocity and Equivalent Airspeed of an airplane

Calculate
Reservoir Pressure, Temperature area ratio for supersonic wind
tunnel

Calculate
Pressure, temperature and density at the stagnation point

Calculate
Velocity at exit and mass flow through the nozzle

Calculate
Velocity at a point on an airfoil

Calculate Mach Number

Calculate Mach
Number of the flow at the nozzle and exit

Calculate True and
Calibrated Airspeed

Calculate
Pressure measured by a Pitot Tube

Calculate
Boundary layer thickness at trailing edge, Drag force on plate
(laminar and turbulent flow)

Calculate
local shear stress in the flow direction (laminar and turbulent
flow)
Planform Analysis
is a basiclanguage based program that carries out the basic geometry
for aerodynamics.
Simple Lifting
Line Theory is a simple Fortran based code that solves the Prandtl
lifting line theory using the monoplane equation.
Induced Drag for
Single Planar Wing
Induced Drag for a
single planar wing is a computer program that uses spanload distribution
to calculate the induced drag for a single planar wing.
Induced Drag for
Nonplanar Lifting elements
This computer
program is able to calculate the induced drag fro nonplanar lifting
elements.
Minimum Drag and
Area Distribution (MinDrag) is a computer program that calculates the
minimum value for supersonic wave drag.
AWave is a Harris
wave drag computation code.
VLMpc is a Vortex
lattice design and analysis program developed at the NASA langely.
Tornado is a
vortex lattice analysis code and is a vortex lattice program written in
Matlab.
AVL (Extended
Vortex Lattice) or AVL shortly is a very powerful and useful vortex
lattice program that can handle a wide variety of geometries and shapes.
XFoil is a
subsonic airfoil analysis and design software that is very powerful and
useful for airfoil design and analysis. It also includes viscous effects
(of airfoils) and can be used in inverse mode to find out the required
geometry by inputting in the pressure distribution. Xfoil author Prof.
Mark Drela is also the author of AVL vortex lattice program.
Arrow calculates
the aerodynamic center, drag due to lift and the lift curve slope of
wings at supersonic speeds.
Aerocal Pak # 1 is
a basic program that calculates the basic aerodynamic relations.
MaxRamp is a
fortran program which calculates the maximum deflection angle of obligue
shockwaves.
Turbsf is a
fortran program which calculates the turbulent skin friction.
Zonatech develops software with specialization and experience in structural dynamics, aerodynamics and Aeroelasticity.
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