If you want to examine some of the codes and documents in this collection, I have placed a few on the web site so you can download them.
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 |