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Public Domain Aeronautical Software (PDAS)  

There are a number of important NACA or NASA reports that are fundamental references for the software in this collection. Some of these are available for downloading from a NASA server or from Public Domain Aeronautical software. They are all on the CD-ROM.

Number Size,KB Description
NACA Rep. 1135 12900 Equations, Charts and Tables for Supersonic Flow
NASA TM 4741 293 1996 revision of the definition of the NACA airfoil sections.
NACA Rep. 411 642 Theodorsen, Theory of wing sections of arbitrary shape
NACA Rep. 452 2361 Theodorsen and Garrick, General potential theory of arbitrary wing section
NACA Rep. 460 4486 Jackson, Ward and Pinkerton, The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel
NACA Rep. 492 1338 Stack and von Doenhoff, Tests of 16 related airfoils at high speed
NACA Rep. 537 701 Jacobs and Pinkerton, Tests in the variable-density wind tunnel of related airfoils having the maximum camber unusually far forward
NACA Rep. 763 946 Stack, Tests of airfoils designed to delay the compressibility burble
NACA Rep. 824 19530 Abbott,Von Doenhoff,Stivers, Summary of airfoil data
NACA Rep. 903 1538 Loftin, Theoretical and experimental data for a number of NACA 6A-series airfoil sections
NASA TM X-3572 67 FLUID, description of the program
NASA TM 85767 396 Description of the NASA Wireframe Geometry Standard
NASA TN D-2987 1288 Flow field in a supersonic inlet

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Public Domain Aeronautical Software (PDAS)