1–20 von 42 Ergebnissen
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    Aerothermodynamic environment for a Titan probe with deployable decelerator

    GREEN, M. / SWENSON, B. / BALAKRISHNAN, A. | AIAA | 1985

    AFT: Aeroelastic Flight Test: NASA - UCLA 1999

    Alvarez-Salazar, O. S. / Balakrishnan, A. V. / Iliff, K. W. | British Library Conference Proceedings | 2001

    Centrifuge Testing of Remediation of Liquefaction at Bridge Sites

    Balakrishnan, A. / Kutter, B.L. / Idriss, I.M. | Transportation Research Record | 1998

    Configuration impact on heat shield requirements for Jupiter entry

    NICOLET, W. / BALAKRISHNAN, A. / MEZINES, S. | AIAA | 1976

    Control of Structures with Self-Straining Actuators: Coupled Euler/Timoshenko Model: I

    Balakrishnan, A. V. | British Library Conference Proceedings | 1999

    Jupiter entry probe afterbody convective heating

    BALAKRISHNAN, A. / CHU, E. | AIAA | 1979

    LQG Optimal Compensator Transfer Function for the NASA LaRC CSI Evolutionary Model

    Balakrishnan, A. V. / National Aeronautics and Space Administration | British Library Conference Proceedings | 1994