Showing 1 - 20 results of 24 for search 'Czarnecki, K. R.', query time: 0.10s Refine Results
  1. 1
    An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds /

    An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds / by Czarnecki, K. R.

    Published 1950
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  2. 2
    An extension of the investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 /

    An extension of the investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1954
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  3. 3
    Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 /

    Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1954
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  4. 4
    Investigation of distributed surface roughness on a body of revolution at a Mach number of 1.61 /

    Investigation of distributed surface roughness on a body of revolution at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1954
    Government Document Book
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  5. 5
    A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61 /

    A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1957
    Government Document Book
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  6. 6
    Effects of fabrication-type roughness on turbulent skin friction at supersonic speeds /

    Effects of fabrication-type roughness on turbulent skin friction at supersonic speeds / by Czarnecki, K. R.

    Published 1958
    Government Document Book
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  7. 7
    Effects of nose angle and Mach number on transition on cones at supersonic speeds /

    Effects of nose angle and Mach number on transition on cones at supersonic speeds / by Czarnecki, K. R.

    Published 1958
    Government Document Book
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  8. 8
    Pressure-drop characteristics of orifice plates used to simulate radiators /

    Pressure-drop characteristics of orifice plates used to simulate radiators / by Czarnecki, K. R.

    Published 1942
    Government Document Book
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  9. 9
    Wind-tunnel investigation of rear underslung fuselage ducts /

    Wind-tunnel investigation of rear underslung fuselage ducts / by Czarnecki, K. R.

    Published 1943
    Government Document Book
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  10. 10
    Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine /

    Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine / by Czarnecki, K. R.

    Published 1946
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  11. 11
    Theoretical pressure distributions over arbitrarily shaped periodic waves in subsonic compressible flow, and comparison with experiment /

    Theoretical pressure distributions over arbitrarily shaped periodic waves in subsonic compressible flow, and comparison with experiment / by Czarnecki, K. R.

    Published 1970
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  12. 12
    Dynamometer-stand investigation of the muffler used in the demonstration of light-airplane noise reduction /

    Dynamometer-stand investigation of the muffler used in the demonstration of light-airplane noise reduction / by Czarnecki, K. R.

    Published 1948
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  13. 13
    Roughness drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder from force tests at transonic speeds /

    Roughness drag due to two-dimensional fabrication-type surface roughness on an ogive cylinder from force tests at transonic speeds / by Czarnecki, K. R., Monta, William J.

    Published 1969
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  14. 14
    Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds /

    Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / by Jackson, Mary W., Czarnecki, K. R.

    Published 1960
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  15. 15
    Drag due to two-dimensional surface roughness in a turbulent boundary layer Mach 3 with and without heat transfer /

    Drag due to two-dimensional surface roughness in a turbulent boundary layer Mach 3 with and without heat transfer / by Monta, William J., Czarnecki, K. R., Deveikis, William D.

    Published 1968
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  16. 16
    Investigation of boundary-layer transition on 10 degree cone in Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 /

    Investigation of boundary-layer transition on 10 degree cone in Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 / by Sinclair, Archibald R.

    Published 1956
    Other Authors: “…Czarnecki, K. R.…”
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  17. 17
    An exploratory investigation of skin friction and transition on three bodies of revolution at a Mach number of 1.61 /

    An exploratory investigation of skin friction and transition on three bodies of revolution at a Mach number of 1.61 / by Hilton, John H.

    Published 1954
    Other Authors: “…Czarnecki, K. R.…”
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  18. 18
    Investigation of effects of distributed surface roughness on a turbulent boundary layer over a body of revolution at a Mach number of 2.01 /

    Investigation of effects of distributed surface roughness on a turbulent boundary layer over a body of revolution at a Mach number of 2.01 / by Sevier, John R.

    Published 1958
    Other Authors: “…Czarnecki, K. R.…”
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  19. 19
    Preliminary data at a Mach number of 2.40 of the characteristics of flap-type controls equipped with plain overhang balances /

    Preliminary data at a Mach number of 2.40 of the characteristics of flap-type controls equipped with plain overhang balances / by Mueller, James N.

    Published 1957
    Other Authors: “…Czarnecki, K. R.…”
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  20. 20
    Wind-tunnel investigation of carburetor-air inlets /

    Wind-tunnel investigation of carburetor-air inlets / by Nelson, W. J.

    Published 1942
    Other Authors: “…Czarnecki, K. R.…”
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