Online Books by
Cornelius Driver
Books from the extended shelves:
![[X-Info]](https://onlinebooks.library.upenn.edu/infouc.gif)
Driver, Cornelius: Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 (National Aeronautics and Space Administration, 1959), also by Langley Research Center (page images at HathiTrust)- Driver, Cornelius: Effects of forebody length on the stability and control characteristics at a Mach number of 2.01 of a canard airplane configuration with a trapezoidal aspect-ratio-3 wing (National Aeronautics and Space Administration :, 1962), also by M. Leroy Spearman and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Driver, Cornelius: Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 degree delta wing (National Aeronautics and Space Administration, 1960), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Driver, Cornelius: Progress in supersonic cruise aircraft technology (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Driver, Cornelius: Stability and control characteristics at a mach number of 2.01 of a supersonic VTOL airplane model having a broad fuselage and small delta wings (National Aeronautics and Space Administration, 1961), also by M. Leroy Spearman and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Driver, Cornelius: Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01 (National Aeronautics and Space Administration, 1959), also by M. Leroy Spearman and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Driver, Cornelius: Tabulated data from a pressure-distribution investigation at mach number 2.01 of the wing of a canard airplane model (National Aeronautics and Space Administration, 1959), also by James L. Jacocks and Langley Research Center (page images at HathiTrust)
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