Preignition-limited Performance of Several Fuels
| Author | : Donald R. Bellman |
| Publisher | : |
| Total Pages | : 210 |
| Release | : 1945 |
| Genre | : Aeronautics |
| ISBN | : |
Preignition Limited Performance Of Several Fuels
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Technical Note - National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 456 |
| Release | : 1946 |
| Genre | : Aeronautics |
| ISBN | : |
Annual Report - National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : |
| Release | : 1945 |
| Genre | : Aeronautics |
| ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Report - National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 752 |
| Release | : 1945 |
| Genre | : Aeronautics |
| ISBN | : |
Wartime Report E.
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 224 |
| Release | : |
| Genre | : Airplanes |
| ISBN | : |
Index of NACA Technical Publications
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1370 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
Wartime Report
| Author | : |
| Publisher | : |
| Total Pages | : 766 |
| Release | : 194? |
| Genre | : Aeronautics |
| ISBN | : |
Reproductions of reports, some declassified, of research done at Aircraft Engine Research Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Effect of Small Deviations from Flatness on Effective Width and Buckling of Plates in Compression
| Author | : Pai C. Hu |
| Publisher | : |
| Total Pages | : 544 |
| Release | : 1946 |
| Genre | : Buckling (Mechanics) |
| ISBN | : |
(3) The Southwell plot method of predicting theoretical critical stresses for perfect specimens from experimental observations on actual specimens may not be expected to give, in general, satisfactory results when applied to flat plates.
