Showing 1 - 9 results of 9 for search '"United States Army"', query time: 2.38s Refine Results
  1. 1
    As soldiers see it,

    As soldiers see it,

    Published 1943
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  2. 2
    Axial-torsional fatigue : a study of tubular specimen thickness effects /

    Axial-torsional fatigue : a study of tubular specimen thickness effects / by Bonacuse, Peter J., 1960-, Kalluri, Sreeramesh

    Published 1990
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  3. 3
    Implementation of an intelligent control system /

    Implementation of an intelligent control system / by Simon, D. L., Wong, E., Musgrave, J. L.

    Published 1992
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  4. 4
    Fracture mechanics of matrix cracking and delamination in glass/epoxy laminates /

    Fracture mechanics of matrix cracking and delamination in glass/epoxy laminates / by Caslini, M., Zanotti, C., O'Brien, T. Kevin

    Published 1986
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  5. 5
    Final programmatic environmental impact statement. Wallops Flight Facility Shoreline Restoration and Infrastructure Protection Program /

    Final programmatic environmental impact statement. Wallops Flight Facility Shoreline Restoration and Infrastructure Protection Program /

    Published 2010
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  6. 6
    Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests /

    Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests / by Yeager, William T., Hamouda, M-Nabil H., Mantay, Wayne R.

    Published 1983
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  7. 7
    Calculation of three-dimensional unsteady transonic flows past helicopter blades /

    Calculation of three-dimensional unsteady transonic flows past helicopter blades / by Chattot, J. J.

    Published 1980
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  8. 8
    Fatigue debonding characterization in composite skin/stringer configurations /

    Fatigue debonding characterization in composite skin/stringer configurations / by Cvitkovich, Michael, O'Brien, T. Kevin, Minguet, Pierre Jacques

    Published 1997
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  9. 9
    Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

    Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / by Noonan, Kevin W., Bingham, Gene J.

    Published 1980
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