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Online Books by

Emma Jean Landrum

Books from the extended shelves:

• Landrum, Emma Jean: 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 K. R. Czarnecki and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 (National Aeronautics and Space Administration, 1960), also by Langley Research Center (page images at HathiTrust)
• Landrum, Emma Jean: Fin loads and tip-control hinge moments on a 1/8-scale model simulating the first stage of the Scout research vehicle at a mach number of 2.01 (National Aeronautics and Space Administration, 1960), also by Ross B. Robinson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: NASA TN D-1867 (National Aeronautics and Space Administration :, 1964), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: 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 K. R. Czarnecki and Langley Research Center (page images at HathiTrust)
• Landrum, Emma Jean: 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 K. R. Czarnecki and Langley Research Center (page images at HathiTrust)
• Landrum, Emma Jean: A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes. Emma Jean Landrum. (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for a reflex cambered wing and a cambered and twisted wing having the same swept planform (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: Theoretical and experimental study of twisted and cambered delta wings designed for a mach number of 3.5 (National Aeronautics and Space Administration ;, 1976), also by Russell B. Sorrells, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landrum, Emma Jean: Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by C. Donald Babb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Landrum, Emma Jean: Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)

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