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Books about K. R. Czarnecki -- Books by K. R. Czarnecki

Books about K. R. Czarnecki:

Books by K. R. Czarnecki:

Books in the extended shelves:

• Czarnecki, K. R.: Effect of fabrication-type surface roughness on transition on ogive-cylinder models at Mach number of 1.61 and 2.01 (National Aeronautics and Space Administration :, 1963), also by Paul W. Howard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Czarnecki, K. R.: Effect of nose bluntness on transition for a cone and a hollow cylinder at mach numbers 1.41 and 2.01 (National Aeronautics and Space Administration :, 1961), also by William J. Monta, Paul W. Howard, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Czarnecki, K. R.: Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform (National Aeronautics and Space Administration :, 1961), also by Emma Jean Landrum and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Czarnecki, K. R.: Effects of cone angel, mach number, and nose blunting on transition at supersonic speeds (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Czarnecki, K. R.: Factors affecting transition at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by Archibald R. Sinclair, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Czarnecki, K. R.: Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds (National Aeronautics and Space Administration, 1960), also by Mary W. Jackson and Langley Research Center (page images at HathiTrust)
• Czarnecki, K. R.: Investigation of effects of roughness, surface cooling, and shock impingement on boundary-layer transition on a two-dimensional wing (National Aeronautics and Space Administration :, 1960), also by John R. Sevier and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Czarnecki, K. R.: Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine (National Advisory Committee for Aeronautics, 1946), also by Jerome Pasamanick and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Czarnecki, K. R.: Load distributions associated with controls at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by Douglas R. Lord, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Czarnecki, K. R.: Loads associated with spoilers at supersonic speeds (National Advisory Committee for Aeronautics, 1955), also by Douglas R. Lord, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Czarnecki, K. R.: NASA TN D-2048 (National Aeronautics and Space Administration, 1963), also by William J. Monta, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Czarnecki, K. R.: NASA TN D-3589 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1966), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Czarnecki, K. R.: NASA TN D-4401 (National Aeronautics and Space Administration ;, 1968), also by Russell B. Sorrells, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Czarnecki, K. R.: NASA TN D-4746 (National Aeronautics and Space Administration :, 1968), also by William J. Monta, William D. Deveikis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Czarnecki, K. R.: NASA TN D-5307 (National Aeronautics and Space Administration ;, 1969), also by Russell B. Sorrells, Lorraine F. Satchell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Czarnecki, K. R.: Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 (National Advisory Committee for Aeronautics, 1952), also by Archibald R. Sinclair, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Czarnecki, K. R.: Pressure distributions and aerodynamic characteristics of several spoiler controls on a 40 degree sweptback wing at a Mach number of 1.61 (National Aeronautics and Space Administration, 1960), also by Emma Jean Landrum and Langley Research Center (page images at HathiTrust)
• Czarnecki, K. R.: Pressure distributions and wave drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder at mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration :, 1961), also by William J. Monta and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Czarnecki, K. R.: Recent information on flap and tip controls (National Advisory Committee for Aeronautics, 1953), also by Douglas R. Lord, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Czarnecki, K. R.: Span loadings and aerodynamic characteristics for a series of tip and trailing-edge controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1959), also by Douglas R. Lord and Langley Research Center (page images at HathiTrust)
• Czarnecki, K. R.: Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40 degree sweptback wing at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1962), also by Emma Jean Landrum and Langley Research Center (page images at HathiTrust)
• Czarnecki, K. R.: Theoretical face pressure and drag characteristics of forward-facing steps in supersonic turbulent boundary layers (National Aeronautics and Space Administration, 1975), also by D. K. Patel (page images at HathiTrust)
• Czarnecki, K. R.: Theoretical pressure distributions over arbitrarily shaped periodic waves in subsonic compressible flow, and comparison with experiment (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), also by Mary W. Jackson (page images at HathiTrust; US access only)

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