Showing 1 - 20 results of 35 for search 'Lomax, Harvard', query time: 0.10s Refine Results
  1. 1
    Generalized conical-flow fields in supersonic wing theory /

    Generalized conical-flow fields in supersonic wing theory / by Lomax, Harvard

    Published 1951
    Government Document Book
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  2. 2
    Three-dimensional unsteady lift problems in high-speed flight : the triangular wing /

    Three-dimensional unsteady lift problems in high-speed flight : the triangular wing / by Lomax, Harvard

    Published 1951
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  3. 3
    The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds /

    The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds / by Lomax, Harvard

    Published 1951
    Government Document Book
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  4. 4
    Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts /

    Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts / by Lomax, Harvard

    Published 1950
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  5. 5
    Formulas for source, doublet, and vortex distributions in supersonic wing theory /

    Formulas for source, doublet, and vortex distributions in supersonic wing theory / by Lomax, Harvard

    Published 1950
    Government Document Book
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  6. 6
    Chordwise and compressibility corrections to slender-wing theory /

    Chordwise and compressibility corrections to slender-wing theory / by Lomax, Harvard

    Published 1951
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  7. 7
    Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations /

    Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations / by Lomax, Harvard

    Published 1951
    Government Document Book
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  8. 8
    Wing-body combinations with certain geometric restraints having low zero-lift wave drag at low supersonic Mach numbers /

    Wing-body combinations with certain geometric restraints having low zero-lift wave drag at low supersonic Mach numbers / by Lomax, Harvard

    Published 1956
    Government Document Book
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  9. 9
    Generalized indicial forces on deforming rectangular wings in supersonic flight /

    Generalized indicial forces on deforming rectangular wings in supersonic flight / by Lomax, Harvard

    Published 1954
    Government Document Book
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  10. 10
    A method for the calculation of wave drag on supersonic-edged wings and biplanes /

    A method for the calculation of wave drag on supersonic-edged wings and biplanes / by Lomax, Harvard

    Published 1958
    Government Document Book
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  11. 11
    Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds /

    Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds / by Lomax, Harvard

    Published 1953
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  12. 12
    Stable implicit and explicit numerical methods for integrating quasi-linear differential equations with parasitic-stiff and parasitic-saddle eigenvalues /

    Stable implicit and explicit numerical methods for integrating quasi-linear differential equations with parasitic-stiff and parasitic-saddle eigenvalues / by Lomax, Harvard

    Published 1968
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  13. 13
    Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations /

    Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations / by Lomax, Harvard

    Published 1949
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  14. 14
    Linearized lifting-surface theory for swept-back wings with slender plan forms /

    Linearized lifting-surface theory for swept-back wings with slender plan forms / by Lomax, Harvard

    Published 1949
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  15. 15
    Two-dimensional, supersonic, linearized flow with heat addition /

    Two-dimensional, supersonic, linearized flow with heat addition / by Lomax, Harvard

    Published 1959
    Government Document Book
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  16. 16
    An operational unification of finite difference methods for the numerical integration of ordinary differential equations /

    An operational unification of finite difference methods for the numerical integration of ordinary differential equations / by Lomax, Harvard

    Published 1967
    Government Document Book
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  17. 17
    Numerical analysis of flow properties about blunt bodies moving at supersonic speeds in an equilibrium gas /

    Numerical analysis of flow properties about blunt bodies moving at supersonic speeds in an equilibrium gas / by Lomax, Harvard

    Published 1964
    Government Document Book
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  18. 18
    Eigensystem analysis of classical relaxation techniques with applications to multigrid analysis

    Eigensystem analysis of classical relaxation techniques with applications to multigrid analysis by Lomax, Harvard

    Published 1987
    Government Document Microfilm Book
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  19. 19
    Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow /

    Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow / by Lomax, Harvard

    Published 1949
    Government Document Book
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  20. 20
    Sideslip angles and vertical-tail loads developed by periodic control deflections /

    Sideslip angles and vertical-tail loads developed by periodic control deflections / by Lomax, Harvard

    Published 1948
    Government Document Book
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