The Online Books Page

Books by James A. Albers:

Books in the extended shelves:

• Albers, James A.: Aerodynamic analysis of several high throat Mach number inlets for the Quiet Clean Short-Haul Experimental Engine (National Aeronautics and Space Administration ;, 1975), also by John J. Hirn, Norbert O. Stockman, and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Boundary-layer analysis of subsonic inlet diffuser geometries for engine nacelles (National Aeronautics and Space Administration ;, 1974), also by E. John Felderman and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Comparison of experimental and theoretical boundary-layer separation for inlets at incidence angle at low-speed conditions (National Aeronautics and Space Administration ;, 1975), also by E. John Felderman and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Computer program for calculating laminar, transitional, and turbulent boundary layers for a compressible axisymmetric flow (National Aeronautics and Space Administration ;, 1974), also by John L. Gregg and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Conditioning and steady-state performance of SNAP-8 tube-in-shell mercury boiler (National Aeronautics and Space Administration ;, 1967), also by Sol H. Gorland, William T. Wintucky, and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions (National Aeronautics and Space Administration ;, 1973), also by Brent A. Miller and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Experimental pressure drop investigation of wetting and nonwetting mercury condensing in uniformly tapered tubes (National Aeronautics and Space Administration ;, 1966), also by Henry B. Block and Lewis Research Center (page images at HathiTrust)
• Albers, James A.: NASA TN D-6394 (National Aeronautics and Space Administration :, 1971), also by Merle C. Potter, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Albers, James A.: Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions (National Aeronautics and Space Administration ;, 1973), also by Lewis Research Center (page images at HathiTrust)
• Albers, James A.: Theoretical surface velocity distributions on acoustic splitter geometries for an engine inlet (National Aeronautics and Space Administration ;, 1974), also by Douglas C. Breunlin and Lewis Research Center (page images at HathiTrust)

Find more by James A. Albers at your library, or elsewhere.