The Online Books Page

Delta wings

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• Analytical investigation of effect of spin entry technique on spin and recovery characteristics for a 60 degree delta-wing airplane (National Aeronautics and Space Administration, 1959), by Stanley H. Scher, George F. Lawrence, Ernie L. Anglin, and Langley Research Center (page images at HathiTrust)
• Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model (National Aeronautics and Space Administration, 1960), by Lewis R. Fisher and Langley Research Center (page images at HathiTrust)
• Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile (National Aeronautics and Space Administration, 1960), by Eugene D. Schult and Langley Research Center (page images at HathiTrust)
• Analysis of the dynamic lateral stability of a delta-wing airplane with frequency-dependent stability derivatives (National Aeronautics and Space Administration, 1959), by Albert E. Brown, Albert A. Schy, and Langley Research Center (page images at HathiTrust)
• Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46 (National Aeronautics and Space Administration, 1959), by Frank J. Centolanzi and Ames Research Center (page images at HathiTrust)
• Trim drag at supersonic speeds of various delta-planform configurations (National Aeronautics and Space Administration, 1960), by M. E. Graham, B. M. Ryan, and Douglas Aircraft Company (page images at HathiTrust)
• Investigation of methods for computing flutter characteristics of supersonic delta wings and comparison with experimental data (National Aeronautics and Space Administration, 1959), by Charles H. Wilts and California Institute of Technology (page images at HathiTrust)
• Measured and predicted section wave drag coefficients at a Mach number of 1.6 for a delta wing with two airfoil sections (National Aeronautics and Space Administration, 1959), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.