Online Books by
William Mulcay
Books from the extended shelves:
![[X-Info]](https://onlinebooks.library.upenn.edu/infouc.gif)
Mulcay, William: Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Julio Chu, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)- Mulcay, William: Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Robert A. Rose, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Mulcay, William: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William Bihrle, Robert Rose, Randy S. Hultberg, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Mulcay, William: Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊ II, High-wing model A (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Robert A. Rose, Langley Research Center, and Inc Bihrle Applied Research (page images at HathiTrust)
- Mulcay, William: 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William Bihrle, Langley Research Center, and Inc Bihrle Applied Research (page images at HathiTrust)
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