| Title: | Prediction of unsteady aerodynamic loadings on non-planar wings and wing-tail configurations in supersonic flow. Part II, Computer program description |
| Author: | Kramer, Gordon D. |
| Author: | Keylon, George E. |
| Author: | United States. Air Force. Systems Command |
| Author: | Air Force Flight Dynamics Laboratory (U.S.) |
| Author: | Boeing Company. Commercial Airplane Group |
| Note: | Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972 |
| 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 load |
| Subject: | Aerodynamics, Supersonic |
| Subject: | Airplanes -- Control surfaces |
| Subject: | Airplanes -- Tail surfaces |
| Subject: | Airplanes -- Wings, Swept-back |
| Subject: | Unsteady flow (Aerodynamics) |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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