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title: National Advisory Committee for Aeronautics -- Reports
Linearized compressible-flow theory for sonic flight speeds
Linearized compressible-flow theory for sonic flight speeds
Calculation of downwash behind supersonic wings with application to triangular plan forms
Volterra's solution of wave equation as applied to three-dimensional supersonic airfoil problems
Formulas for source, doublet, and vortex distributions in supersonic wing theory
Linearized lifting-surface theory for swept-back wings with slender plan forms
Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations
Calculation of pressure on slender airplanes in subsonic and supersonic flow
Chordwise and compressibility corrections to slender-wing theory
Chordwise and compressibility corrections to slender-wing theory
Integrals and integral equations in linearized wing theory
Calculation of downwash behind supersonic wings with application to triangular plan forms
Downwash in vertical and horizontal planes of symmetry behind triangular wing in supersonic flow
Three-dimensional, unsteady-lift problems in high-speed flight -- Basic concepts
Three-dimensional unsteady lift problems in high-speed flight -- Triangular wing
Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds