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  1. 1
    Pressure distribution and damping in steady pitch at supersonic Mach numbers of flat swept-back wings having all edges subsonic /

    Pressure distribution and damping in steady pitch at supersonic Mach numbers of flat swept-back wings having all edges subsonic / by Walker, Harold J.

    Published 1950
    Government Document Book
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  2. 2
    Energy transfer from a test electron to a collisionless plasma /

    Energy transfer from a test electron to a collisionless plasma / by Kelley, Joseph G.

    Published 1966
    Government Document Book
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  3. 3
    The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds /

    The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds / by Cooper, Morton

    Published 1951
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  4. 4
    Comparison of theoretical and experimental heat transfer on a cooled 20 degree cone with a laminar boundary layer at a Mach number of 2.02 /

    Comparison of theoretical and experimental heat transfer on a cooled 20 degree cone with a laminar boundary layer at a Mach number of 2.02 / by Scherrer, R.

    Published 1950
    Government Document Book
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  5. 5
    Data on shape and location of detached shock waves on cones and spheres /

    Data on shape and location of detached shock waves on cones and spheres / by Heberle, Juergen W.

    Published 1949
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  6. 6
    Boundary-layer transition on a cooled 20° cone at Mach numbers of 1.5 and 2.0 /

    Boundary-layer transition on a cooled 20° cone at Mach numbers of 1.5 and 2.0 / by Scherrer, R.

    Published 1950
    Government Document Book
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  7. 7
    Some conical and quasi-conical flows in linearized supersonic-wing theory /

    Some conical and quasi-conical flows in linearized supersonic-wing theory / by Ribner, H. S. (Herbert S.), 1913-

    Published 1950
    Government Document Book
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  8. 8
    Theoretical aerodynamic characteristics of bodies in a free-molecule-flow field /

    Theoretical aerodynamic characteristics of bodies in a free-molecule-flow field / by Stalder, Jackson R.

    Published 1951
    Government Document Book
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  9. 9
    Flow separation ahead of blunt bodies at supersonic speeds /

    Flow separation ahead of blunt bodies at supersonic speeds / by Moeckel, W. E. (Wolfgang E.)

    Published 1951
    Government Document Book
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  10. 10
    Supersonic flow around circular cones at angles of attack /

    Supersonic flow around circular cones at angles of attack / by Ferri, Antonio, 1912-1975

    Published 1950
    Government Document Book
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  11. 11
    An approximate solution for axially symmetric flow over a cone with an attached shock wave /

    An approximate solution for axially symmetric flow over a cone with an attached shock wave / by Hord, Richard A.

    Published 1955
    Government Document Book
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  12. 12
    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
    Government Document Book
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  13. 13
    Stability derivatives of cones at supersonic speeds /

    Stability derivatives of cones at supersonic speeds / by Tobak, Murray

    Published 1956
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  14. 14
    Generalized linearized conical flow /

    Generalized linearized conical flow / by Hayes, W. D.

    Published 1952
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  15. 15
    Use of the boundary layer of a cone to measure supersonic flow inclination /

    Use of the boundary layer of a cone to measure supersonic flow inclination / by Moore, F. K. (Franklin K.)

    Published 1952
    Government Document Book
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  16. 16
    The calculation of pressure on slender airplanes in subsonic and supersonic flow /

    The calculation of pressure on slender airplanes in subsonic and supersonic flow / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1953
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  17. 17
    Laminar boundary layer on cone in supersonic flow at large angle of attack /

    Laminar boundary layer on cone in supersonic flow at large angle of attack / by Moore, F. K. (Franklin K.)

    Published 1952
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  18. 18
    Effect of various arrangements of triangular ledges on the performance of a 23 degree conical diffuser at subsonic Mach numbers /

    Effect of various arrangements of triangular ledges on the performance of a 23 degree conical diffuser at subsonic Mach numbers / by Persh, Jerome

    Published 1954
    Government Document Book
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  19. 19
    Theoretical pressure distributions and wave drags for conical boattails /

    Theoretical pressure distributions and wave drags for conical boattails / by Jack, John R.

    Published 1953
    Government Document Book
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  20. 20
    Determination of boundary-layer transition Reynolds numbers by surface-temperature measurement of a 10 degree cone in various NACA supersonic wind tunnels /

    Determination of boundary-layer transition Reynolds numbers by surface-temperature measurement of a 10 degree cone in various NACA supersonic wind tunnels / by Ross, Albert O.

    Published 1953
    Government Document Book
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