The Online Books Page

Books by Kevin W. Noonan:

Books in the extended shelves:

• Noonan, Kevin W.: Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Gene J. Bingham, Army Research and Technology Laboratories (U.S.). Structures Laboratory, United States. Army Aviation Research and Development Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Noonan, Kevin W.: Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by United States. Army Aerostructures Directorate (page images at HathiTrust)
• Noonan, Kevin W.: Effect of blade planform variation on a small-scale hovering rotor (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Susan L. Althoff and United States. Army Aerostructures Directorate (page images at HathiTrust)
• Noonan, Kevin W.: Effect of blade planform variation on the forward-flight performance of small-scale rotors (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by United States. Army. Aeroflightdynamics Directorate (page images at HathiTrust)
• Noonan, Kevin W.: Experimental investigation of three helicopter rotor airfoils designed analytically (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Gene J. Bingham, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Noonan, Kevin W.: Low-speed aerodynamic characteristics of a 16-percent thick variable-geometry airfoil designed for general aviation applications (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Richard W. Barnwell, Robert J. McGhee, Army Research and Technology Laboratories (U.S.). Structures Laboratory, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Noonan, Kevin W.: Low speed aerodynamic characteristics of NACA 6716 and NACA 4416 airfoils with 35 percent-chord single-slotted flaps (National Aeronautics and Space Administration ;, 1974), also by Gene J. Bingham and Langley Research Center (page images at HathiTrust)

Find more by Kevin W. Noonan at your library, or elsewhere.