The Online Books Page

Books by Walter B. Olstad:

Books in the extended shelves:

• Olstad, Walter B.: Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds (National Aeronautics and Space Administration, 1960), also by Langley Research Center (page images at HathiTrust)
• Olstad, Walter B.: NASA TN D-4754 (National Aeronautics and Space Administration :, 1968), also by Roger D. Bengtson, Jane T. Kemper, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Olstad, Walter B.: NASA TN D-5792 (National Aeronautics and Space Administration ;, 1970), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Olstad, Walter B.: NASA TR R-295 (National Aeronautics and Space Administration ;, 1968), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Olstad, Walter B.: Static longitudinal aerodynamic characteristics at transonic speeds and angles of attack up to 99 degree of a reentry glider having folding wing-tip panels (National Aeronautics and Space Administration, 1961), also by Langley Research Center (page images at HathiTrust)
• Olstad, Walter B.: Static longitudinal aerodynamic characteristics at transonic speeds of a blunted right triangular pyramidal lifting reentry configuration for angles of attack up to 110° (National Aeronautics and Space Administration, 1961), also by John P. Mugler (page images at HathiTrust; US access only)
• Olstad, Walter B.: Static longitudinal aerodynamic characteristics at transonic speeds of a lenticular-shaped reentry vehicle (National Aeronautics and Space Administration, 1960), also by John P. Mugler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Olstad, Walter B.: A study of the feasibility of inflatable reentry gliders (National Aeronautics and Space Administration :, 1960) (page images at HathiTrust)
• Olstad, Walter B.: Theoretical evaluation of hypersonic forces moments and stability derivatives for combinations of flat plates, including effects of blunt leading edges, by Newtonian impact theory (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)

Find more by Walter B. Olstad at your library, or elsewhere.