| Title: | Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41 |
| Author: | Coletti, Donald E. |
| Author: | Langley Aeronautical Laboratory |
| Author: | United States. National Adviosry Committee for Aeronautics |
| Note: | National Advisory Committee for Aeronautics, 1954 |
| 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: | Airplanes -- Tail surfaces |
| Subject: | Leading edges (Aerodynamics) |
| Subject: | Rolling (Aerodynamics) |
| Subject: | Trailing edges (Aerodynamics) |
| Subject: | Yawing (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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