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Online Books by

Cuyler W. Brooks

Books from the extended shelves:

• Brooks, Cuyler W.: Development of a computer program to obtain ordinates for NACA 4-digit, 4-digit modified, 5-digit, and 16-series airfoils / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), also by Charles L. Ladson and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: Development of a computer program to obtain ordinates from NACA 6- and 6A-series airfoils / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by Charles L. Ladson and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: Effect of blockage ratio on drag and pressure distributions for bodies of revolution at transonic speeds (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), also by Lana M. Couch, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Brooks, Cuyler W.: The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : design overview / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service,), also by Charles D. Harris, William D. Harvey, and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : drag euqations / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), also by William D. Harvey and Charles D. Harris (page images at HathiTrust)
• Brooks, Cuyler W.: The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), also by William D. Harvey, Charles D. Harris, and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: Static longitudinal aerodynamic characteristics at a Mach number of 10.03 of low-aspect-ratio wing-body configurations suitable for reentry / (Washington, D.C. : National Aeronautics and Space Administration, 1962), also by Lawrence E. Putnam and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: A streamline curvature method for design of supercritical and subcritical airfoils / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by Raymond L. Barger and Langley Research Center (page images at HathiTrust)
• Brooks, Cuyler W.: Transonic investigation of the effects of nose bluntness, fineness ratio, cone angle, and base shape on the static aerodynamic characteristics of short, blunt cones at angles of attack to 180⁰ / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), also by Charles D. Trescot and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Brooks, Cuyler W.: Transonic investigation of the static longitudinal aerodynamic characteristics of low-aspect-ratio wing-body configurations at angles of attack from 0⁰ to 90⁰ / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), also by Charles D. Trescot, Lawrence E. Putman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Brooks, Cuyler W.: Transonic static and dynamic stability characteristics of a finned projectile configuration / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1978), also by Richmond P. Boyden, Edwin E. Davenport, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Brooks, Cuyler W.: Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), also by Thomas A. Byrdsong, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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