Online Books by
John W. Paulson
Books from the extended shelves:
![[X-Info]](https://onlinebooks.library.upenn.edu/infouc.gif)
Paulson, John W.: Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)- Paulson, John W.: Effects of deflected thrust on the longitudinal aerodynamic chartacteristics of a close-coupled wing-canard configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Long P. Yip and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Paulson, John W.: An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect (National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ;, 1982), also by Scott O. Kjelgaard and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Paulson, John W.: Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by P. Frank Quinto and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Paulson, John W.: Investigation of a moving-model technique for measuring ground effects (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), also by Guy T. Kemmerly (page images at HathiTrust)
- Paulson, John W.: Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by (National Aeronautics and Space Administration :, 1961), also by Robert E. Shanks and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Paulson, John W.: Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by (National Aeronautics and Space Administration :, 1961), also by Robert E. Shanks and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Paulson, John W.: Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration (National Aeronautics and Space Administration :, 1961), also by Robert E. Shanks and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Paulson, John W.: Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Daniel W. Banks, P. Frank Quinto, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Paulson, John W.: Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane (National Aeronautics and Space Administration, 1959), also by James L. Hassell and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Paulson, John W.: Low-speed measurements of oscillatory lateral stability derivatives of a model of 60 degree delta-wing bomber (National Aeronautics and Space Administration, 1959), also by Langley Research Center (page images at HathiTrust)
- Paulson, John W.: NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), also by John P. Campbell, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
- Paulson, John W.: A Review of technologies applicable to low-speed flight of high-performance aircraft investigated in the Langley 14- by 22-foot subsonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), also by Langley Research Center (page images at HathiTrust)
- Paulson, John W.: Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by James L. Thomas, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Paulson, John W.: Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by P. Frank Quinto and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
See also what's at your library, or elsewhere.
Help with reading books -- Report a bad link -- Suggest a new listing
Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials
Books -- News -- Features -- Archives -- The Inside Story
Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.