1–16 of 16 hits
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    Linearized compressible-flow theory for sonic flight speeds

    Heaslet, M.A. / Lomax, H. / Spreiter, J.R. | Engineering Index Backfile | 1950
    Partial differential equation for perturbation velocity potential is examined for free stream Mach numbers close to and equal to one. (20¢) ...
    Publisher: National Advisory Committee for Aeronautics

      Linearized compressible-flow theory for sonic flight speeds

      Heaslet, M.A. / Lomax, H. / Spreiter, J.R. | Engineering Index Backfile | 1949
      Partial differential equation for perturbation velocity potential is examined for free stream Mach numbers close to and equal to one. ...
      Publisher: National Advisory Committee for Aeronautics

    Application of green's theorem to solution of boundary-value problems in linearized supersonic wing theory

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

    Calculation of downwash behind supersonic wings with application to triangular plan forms

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

    Volterra's solution of wave equation as applied to three-dimensional supersonic airfoil problems

    Heaslet, M.A. / Lomax, H. / Jones, A.L. | Engineering Index Backfile | 1947
    Publisher: National Advisory Committee for Aeronautics (NACA)

    Formulas for source, doublet, and vortex distributions in supersonic wing theory

    Lomax, H. / Heaslet, M.A. / Fuller, F.B. | Engineering Index Backfile | 1950
    Formulas for source, doublet, and vortex distributions in supersonic wing theory. ...
    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

    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

    Calculation of pressure on slender airplanes in subsonic and supersonic flow

    Heaslet, M.A. / Lomax, H. | Engineering Index Backfile | 1954
    Publisher: National Advisory Committee for Aeronautics

    Chordwise and compressibility corrections to slender-wing theory

    Lomax, H. / Sluder, L. | Engineering Index Backfile | 1952
    Publisher: National Advisory Committee for Aeronautics

      Chordwise and compressibility corrections to slender-wing theory

      Lomax, H. / Sluder, L. | Engineering Index Backfile | 1951
      Method of obtaining corrections; results shown for flat plate, rectangular, and triangular wings. ...
      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

    Calculation of downwash behind supersonic wings with application to triangular plan forms

    Heaslet, M.A. / Lomax, H. | Engineering Index Backfile | 1948
    supersonic flow for known load distribution; analysis based upon use of supersonic doublets distributed over plan form and wake of wing in manner ...
    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

    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

    Three-dimensional unsteady lift problems in high-speed flight -- Triangular wing

    Lomax, H. / Heaslet, M.A. / Fuller, F.B. | Engineering Index Backfile | 1951
    Publisher: National Advisory Committee for Aeronautics

    Wing-body combinations with certain geometric restraints having low zero-lift wave drag at low supersonic mach numbers

    Lomax, H. | Engineering Index Backfile | 1956
    Publisher: National Advisory Committee for Aeronautics

    Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds

    Lomax, H. | Engineering Index Backfile | 1953
    Publisher: National Advisory Committee for Aeronautics