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    BUCKLING CRITERION FOR LINEAR VISCOELASTIC COLUMNS

    DE LEEUW / S. L. | AIAA | 1963

    Whither reliabilityques

    DE S. COUTINHO / J. | AIAA | 1965

    Comments on particle size analysis of ammonium perchlorate by liquid sedimentation

    DE MARCHI / V. S. | AIAA | 1965

    Incompressible laminar axisymmetric near wake behind a very slender cylinder in axial flow.

    BERGER, S. A. | AIAA | 1965

    Effect of base bleeding on the near wake for very low Reynolds numbers.

    BERGER, S. A. | AIAA | 1965

    Spacecraft capillary propellant retention and control for long-life missions

    DE BROCK, S. | AIAA | 1968

    Behavior of the incidence of an accelerated missile with locked controls.

    DE ZUCCOLI / S. | AIAA | 1968

    Synthesis of structural damping.

    BIEBER, R. E. | AIAA | 1968

    Local flow effects on base pressure.

    CASSANTO, J. M. | AIAA | 1968

    Agena propulsion system flight performance prediction

    DE BROCK, S. | AIAA | 1969

    A forecast of air travel and airport and airway use in 1980

    De Vany, Arthur S. / Garges, Eleanor H. | Elsevier | 1971

    A survey of current developments in surface tension devices for propellant acquisition

    BALZER, D. L. / BRILL, Y. | AIAA | 1971

    Aerodynamic characteristics for a slender missile with wrap-around fins

    CATANI, U. / DE AMICIS / R. et al. | AIAA | 1983

    Melting and solidification of metallic composites in space

    Deruyttere, A. / Froyen, L. / De Bondt, S. | Elsevier | 1986

    An empirical model of the F1 intermediate layer true-height characteristics

    González, M.Mosert de / Radicella, S. | Elsevier | 1987

    Large space observatories of the 21st century

    NEIN, M. / HOWELL, J. / MORGAN, S. et al. | AIAA | 1987

    Development and pre-flight testing of the Olympus propulsion subsystem

    DEVEY, R. / GAYDON, S. / STATHAM, G. et al. | AIAA | 1989

    Incompressible steady aerodynamics using a standard finite element code

    DE ROSA / S. / PEZZULLO, G. | AIAA | 1991

    Liquid atomization by coaxial rocket injectors

    SANKAR, S. / BRENA DE LA ROSA, A / ISAKOVIC, A. et al. | AIAA | 1991

    Calculation of the two-phase aft-dome flowfield in solid rocket motors

    MADABHUSHI, RAVI K. / SABNIS, JAYANT S. / DE JONG et al. | AIAA | 1991

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