Showing 1 - 20 results of 20 for search 'Mirels, Harold', query time: 0.08s Refine Results
  1. 1
    Estimate of slip effect on compressible laminar-boundary-layer skin friction /

    Estimate of slip effect on compressible laminar-boundary-layer skin friction / by Mirels, Harold

    Published 1952
    Government Document Book
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  2. 2
    Lift-cancellation technique in linearized supersonic-wing theory /

    Lift-cancellation technique in linearized supersonic-wing theory / by Mirels, Harold

    Published 1950
    Government Document Book
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  3. 3
    Boundary layer behind shock or thin expansion wave moving into stationary fluid /

    Boundary layer behind shock or thin expansion wave moving into stationary fluid / by Mirels, Harold

    Published 1956
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  4. 4
    Acoustic analysis of ram-jet buzz /

    Acoustic analysis of ram-jet buzz / by Mirels, Harold

    Published 1955
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  5. 5
    Laminar boundary layer behind shock advancing into stationary fluid /

    Laminar boundary layer behind shock advancing into stationary fluid / by Mirels, Harold

    Published 1955
    Government Document Book
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  6. 6
    Attenuation in a shock tube due to unsteady-boundary-layer action /

    Attenuation in a shock tube due to unsteady-boundary-layer action / by Mirels, Harold

    Published 1954
    Government Document Book
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  7. 7
    Aerodynamics of slender wings and wing-body combinations having swept trailing edges /

    Aerodynamics of slender wings and wing-body combinations having swept trailing edges / by Mirels, Harold

    Published 1954
    Government Document Book
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  8. 8
    Nonuniformities in shock-tube flow due to unsteady-boundary-layer action /

    Nonuniformities in shock-tube flow due to unsteady-boundary-layer action / by Mirels, Harold

    Published 1957
    Government Document Book
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  9. 9
    Acoustic analysis of ram-jet buzz /

    Acoustic analysis of ram-jet buzz / by Mirels, Harold

    Published 1955
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  10. 10
    Aerodynamics of slender wings and wing-body combinations having swept trailing edges /

    Aerodynamics of slender wings and wing-body combinations having swept trailing edges / by Mirels, Harold

    Published 1954
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  11. 11
    Source distribution method for unsteady one-dimensional flows with small mass, momentum, and heat addition and small area ventilation /

    Source distribution method for unsteady one-dimensional flows with small mass, momentum, and heat addition and small area ventilation / by Mirels, Harold

    Published 1959
    Government Document Book
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  12. 12
    Effect of body perturbations on hypersonic flow over slender power law bodies /

    Effect of body perturbations on hypersonic flow over slender power law bodies / by Mirels, Harold

    Published 1959
    Government Document Book
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  13. 13
    Approximate analytical solutions for hypersonic flow over slender power law bodies /

    Approximate analytical solutions for hypersonic flow over slender power law bodies / by Mirels, Harold

    Published 1959
    Government Document Book
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  14. 14
    Theoretical method for solution of aerodynamic forces on thin wings in nonuniform supersonic stream with an application to tail surfaces /

    Theoretical method for solution of aerodynamic forces on thin wings in nonuniform supersonic stream with an application to tail surfaces / by Mirels, Harold

    Published 1948
    Government Document Book
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  15. 15
    Theoretical wave drag and lift of thin supersonic ring airfoils /

    Theoretical wave drag and lift of thin supersonic ring airfoils / by Mirels, Harold

    Published 1948
    Government Document Book
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  16. 16
    Line-vortex theory for calculation of supersonic downwash /

    Line-vortex theory for calculation of supersonic downwash / by Mirels, Harold

    Published 1949
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  17. 17
    Shock tube test time limitation due to turbulent wall boundary layer /

    Shock tube test time limitation due to turbulent wall boundary layer /

    Published 1963
    Other Authors: “…Mirels, Harold…”
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  18. 18
    Charts for estimating downwash behind rectangular, trapezoidal, and triangular wings at supersonic speeds /

    Charts for estimating downwash behind rectangular, trapezoidal, and triangular wings at supersonic speeds / by Haefeli, Rudolph C.

    Published 1950
    Other Authors: “…Mirels, Harold…”
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  19. 19
    Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002.

    Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002.

    Published 1951
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  20. 20
    Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

    Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

    Published 1952
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