Technical Note - National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1274 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
An Investigation Of A Lifting 10 Percent Thick Symmetrical Double Wedge Airfoil At Mach Up To 1
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Research Abstracts
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 12 |
| Release | : 1952 |
| Genre | : Aeronautics |
| ISBN | : |
Index of NACA Technical Publications
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 580 |
| Release | : 1956 |
| Genre | : Aeronautics |
| ISBN | : |
Research Abstracts and Reclassification Notice
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 508 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
WADC Technical Report
| Author | : United States. Wright Air Development Division |
| Publisher | : |
| Total Pages | : 1430 |
| Release | : 1956 |
| Genre | : Aeronautics |
| ISBN | : |
Charts for Estimating Rotor-blade Flapping Motion of High-performance Helicopters
| Author | : Robert J. Tapscott |
| Publisher | : |
| Total Pages | : 692 |
| Release | : 1956 |
| Genre | : Charts, diagrams, etc |
| ISBN | : |
Theoretically derived charts showing steady-state and first- and second-harmonic flapping coefficients are presented for helicopter rotors having hinged rectangular blades with a linear twist of 0, -8, and -16 degrees. The charts, showing the rotor flapping coefficients for combinations of inflow ratio and blade pitch angle, are presented for tip-speed ratios ranging from 0.05 to 0.50.
NASA Memorandum
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 590 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
