1–5 of 5 hits
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    Three-dimensional, unsteady-lift problems in high-speed flight -- Basic concepts

    Lomax, H. / Heaslet, M.A. / Fuller, F.B. | Engineering Index Backfile | 1950
    Publisher: National Advisory Committee for Aeronautics

    Linearized lifting-surface theory for swept-back wings with slender plan forms

    Lomax, H. / Heaslet, M.A. | Engineering Index Backfile | 1949
    Linearized lifting-surface theory for swept-back wings with slender plan forms. ...
    Publisher: National Advisory Committee for Aeronautics

    Integrals and integral equations in linearized wing theory

    Lomax, H. / Heaslet, M.A. / Fuller, F.B. | Engineering Index Backfile | 1951
    Supersedes NACA -- Tech Note 2252 "Formulas for Source, Doublet, and Vortex Distributions in Supersonic Wing Theory", indexed in ...
    Publisher: National Advisory Committee for Aeronautics

    Downwash in vertical and horizontal planes of symmetry behind triangular wing in supersonic flow

    Lomax, H. / Sluder, L. | Engineering Index Backfile | 1949
    Method developed in Tech Note n 1620 for finding induced velocity field behind supersonic wing with known load distribution is used to find ...
    Publisher: National Advisory Committee for Aeronautics

    Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations

    Lomax, H. / Heaslet, M.A. | Engineering Index Backfile | 1949
    Damping-In-Roll Calculations for Slender Swept-Back Wings and Slender Wing-Body Combinations. ...
    Publisher: National Advisory Committee for Aeronautics