Index of NACA Technical Publications
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 580 |
| Release | : 1956 |
| Genre | : Aeronautics |
| ISBN | : |
An Investigation Of The Low Speed Longitudinal Stability Characteristics Of A Swept Wing Airplane Model With Two Modifications To The Wing Root Plan Form
Download An Investigation Of The Low Speed Longitudinal Stability Characteristics Of A Swept Wing Airplane Model With Two Modifications To The Wing Root Plan Form full books in PDF, epub, and Kindle. Read online free An Investigation Of The Low Speed Longitudinal Stability Characteristics Of A Swept Wing Airplane Model With Two Modifications To The Wing Root Plan Form ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Research Abstracts and Reclassification Notice
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 508 |
| Release | : 1954 |
| Genre | : Aeronautics |
| ISBN | : |
Monthly Catalog of United States Government Publications
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 2106 |
| Release | : 1959 |
| Genre | : Government publications |
| ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3
| Author | : Allen B. Henning |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1957 |
| Genre | : Aerofoils |
| ISBN | : |
An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.
NASA Scientific and Technical Reports
| Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 2300 |
| Release | : 1967 |
| Genre | : Aeronautics |
| ISBN | : |
A Selected Listing of NASA Scientific and Technical Reports for 1966
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 2084 |
| Release | : 1967 |
| Genre | : Aeronautics |
| ISBN | : |
Research Abstracts
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 442 |
| Release | : |
| Genre | : Aeronautics |
| ISBN | : |
