| Title: | Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 35.̊ III, Effect of wing leading-edge modifications model A |
| Author: | Bihrle, William |
| Author: | Mulcay, William |
| Author: | Langley Research Center |
| Author: | Bihrle Applied Research, Inc |
| Note: | National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979 |
| 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 measurements |
| Subject: | Leading edges (Aerodynamics) |
| Subject: | Private planes |
| Subject: | Spin (Aerodynamics) |
| Subject: | Wind tunnel balances |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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