Public Domain Aeronautical Software (PDAS)
There are a number of programs in the PDAS archives that appear to be of
some value, but are lacking in some of the requirements for general release.
I have decided to make these codes available for downloading and inspection
by the aeronautical community.
Each code has a reference page with some additional information.
In some cases, the program compiles and seems to run, but there are no
instructions or references available.
The name in bold type following the slash in each program description
is the name of the folder on the CD where the files for this program will be found.
-
Analytical comparisons of ablative nozzle materials / ABLATE
- Atmospheric interaction plume program / AIPP
- Velocity in an annular duct / ANDUCT
- Three-Dimensional Supersonic Viscous Flow (AOFA) / AOFA
-
Aircraft roll-out iterative energy simulation program / ARIES
- Nonrotating Blade-To-Blade, Steady, Potential Transonic
Cascade Flow Analysis Code / CAS2D
-
Dissociated air flow effects during plasma arc testing / COLDARC
- Generalized digital contouring program / CONTOUR
-
A General Algorithm For The Construction Of Contour Plots / CONPLOT
-
Conical relaxation program for supersonic wing design and analysis / COREL
-
Aeroelastic divergence characteristics of unguided, slender body,
multi-stage launch vehicles / DIVERGE
- Static aeroelastic program / ELASTIC
-
Analysis of three-dimensional supersonic nozzle exhaust flow fields / EXHAUST
- Flexible spacecraft dynamics / FSD
- A General Optical Systems Evaluation Program / GOPTICS
- Hypersonic Aerodynamics / HYPER
- Improved Price Estimation Guidelines / IPEG
- LONGLIB - A Graphics Library / LONGLIB
- Aerodynamic Lift On Wing-Body Combinations At Small Angles Of
Attack In Supersonic Flow / MISLIFT
-
Monte Carlo Investigation Of Trajectory Operations And Requirements
/ MONITOR
- NASTRAN plotting post processor / NASTPLT
-
A segmented mission analysis program for low and high speed aircraft / NSEG
-
A vertical profile which minimizes aircraft fuel burn or direct
operating cost / OPTIM
- Optimum Trajectory of a Turbofan Airplane / OPTTRAJ
-
Parametrized Investigation of Launch Opportunities and Trajectories / PILOT
-
Design Of Two-Dimensional Supersonic Turbine Rotor Blades With
Boundary-Layer Correction / RBLADE
- Fast Mars Relay Communication Link / RELAY
-
Aeroelastic Analysis For Rotorcraft In Flight Or In A Wind Tunnel / ROTOR
-
Super/hypersonic Inviscid Flow Around Real Configurations / SHIFARC
- Sneak Circuit Analysis / SNEAK
- Space Shuttle Synthesis Program / SSSP
-
Velocities And Streamlines on a Blade-To-Blade Stream Surface of a
Tandem Blade Turbomachine / TANDEM
- Interplanetary Mission Planner / TOMARS
-
One-Dimensional Numerical Analysis Of The Transient Thermal Response
Of Multilayer Insulative Systems / THERM1D
- Multidimensional Heat Conduction Program / TPS
- V/STOL Aircraft Sizing And Performance
/ VASCOMP
- Supersonic Wing Design / W12SC3
- Virtual Reality / VRML
Public Domain Aeronautical Software (PDAS)