| Title: | Wind-tunnel investigation of effect of ratio of wing chord to propeller diameter with addition of slats on the aerodynamic characteristics of tilt-wing VTOL configurations in the transition speed range |
| Author: | Taylor, Robert T., NASA ressearcher |
| Author: | United States. National Aeronautics and Space Administration |
| Author: | Langley Research Center |
| Note: | National Aeronautics and Space Administration, 1959 |
| Link: | page images at HathiTrust |
| No stable link: | This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links. |
| Subject: | Aerodynamic configurations |
| Subject: | Aerodynamic stalling |
| Subject: | Angle of attack |
| Subject: | Chords (geometry) |
| Subject: | Leading edge slats |
| Subject: | Pitching moments |
| Subject: | Propeller blades |
| Subject: | Vertical takeoff aircraft |
| Subject: | Wind tunnel tests |
| Subject: | Wing profiles |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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