1–20 von 26 Ergebnissen
|

    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

    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

    Methods for the analysis of high-pressure, high-enthalpy constrictedarc heaters

    NICOLET, W. / SHEPARD, C. / CLARK, K. et al. | AIAA | 1975

    PLC platform for low-cost optical access components

    Pearson, M. / Bidnyk, S. / Balakrishnan, A. et al. | IEEE | 2005

    Radiation heat transfer in the wake of a hypersonic vehicle

    BABIKIAN, D. / EDWARDS, D. / BALAKRISHNAN, A. et al. | AIAA | 1988

    Radiative viscous-shock-layer analysis of Fire, Apollo, and PAET flight data

    BALAKRISHNAN, A. / PARK, C. / GREEN, M. | AIAA | 1985

    Radiometer experiment for the aeroassist flight experiment

    DAVY, W. / PARK, C. / ARNOLD, J. et al. | AIAA | 1985