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    Measures of modal controllability and observability for first- and second-order linear systems

    HAMDAN, A. M. A. / NAYFEH, A. H. | AIAA | 1989

    OPTIMUM POLAR SATELLITE NETWORKS FOR CONTINUOUS EARTH COVERAGE

    SCHOEN, A. H. / ULLOCK, M. H. | AIAA | 1963

    Film thickness measurements in a simplex swirl atomizer

    LEFEBVRE, A. H. / SUYARI, M. | AIAA | 1986

    Transport Coefficients for High-Temperature Nonequilibrium Air Flows

    M. Fertig / A. Dohr / H.-H. Fr-uacute et al. | AIAA | 2001

    Continuum modeling of three-dimensional truss-like space structures

    NAYFEH, A. H. / HEFZY, M. S. | AIAA | 1978

    Eigenstructure of the State Matrix of Balanced Realizations

    A. M. A. Hamdan / A. H. Nayfeh | AIAA | 1989

    Lee-side vortices on delta wings at hypersonic speeds.

    RAO, D. M. / WHITEHEAD, A. H. | AIAA | 1972

    Performance of a fully mechanical parking brake system for passenger cars

    Freier Zugriff
    Rozaini, A H / Ishak, M R / Bakar, A R Abu et al. | IOP Institute of Physics | 2013

    Closed-loop soft-constrained time-optimal control of flexible space structures

    CLIFF, E. M. / NAYFEH, A. H. / BIKDASH, M. | AIAA | 1992

    Restart transients of hybrid rocket engines.

    SARANIERO, M. A. / CAVENY, L. H. / SUMMERFIELD, M. | AIAA | 1973

    Nonsteady burning phenomena of solid propellants - Theory and experiments.

    KRIER, H. / SIRIGNANO, W. A. / SUMMERFIELD, M. | AIAA | 1968

    Surface pressure measurements on a body subject to vortex wake interaction

    BRAND, A. G. / MCMAHON, H. M. / KOMERATH, N. M. | AIAA | 1989

    Soot Surface Growth in Laminar Hydrocarbon/Air Diffusion Flames

    A. M. El-Leathy / C. H. Kim / G. M. Faeth | AIAA | 2003

    A simple linear approximation for perturbed motion about moderately elliptic orbits

    KOBLE, H. M. / SCHNEIDER, A. M. | AIAA | 1970

    Experimental investigations of the vortex flow on delta wings at high incidence

    STAHL, W. H. / MAHMOOD,M. / ASGHAR, A. | AIAA | 1992

    Saturating and time-optimal feedback controls

    BIKDASH, M. / CLIFF, E. M. / NAYFEH, A. H. | AIAA | 1993

    Flame stabilization in high-velocity heterogeneous fuel-air mixtures

    BAXTER, M. R. / LEFEBVRE, A. H. | AIAA | 1992

    Vorticity Measurements Using Calibrated Vane-Vorticity Indicators and Cross-Wires

    R. A. Wigeland / M. Ahmed / H. M. Nagib | AIAA | 1978

    Vortex-fitted potential and vortex-captured Euler solution for leading-edge vortex flow

    HOEIJMAKERS, H. W. M. / RIZZI, A. | AIAA | 1985

    Fluid-Structure Interaction Dynamics in Aircraft Fuel Tanks

    M. A. Ferman / W. H. Unger | AIAA | 1979

    Comparative Performance Study of Paddle- and Wedge-Type Wave Generators

    M. H. Patel / P. A. Ionnaou | AIAA | 1980

    Management of Swirling Flows with Application to Wind Tunnel Design

    R. A. Wigeland / M. Ahrned / H. M. Nagib | AIAA | 1978

    Modeling Turbulence in the Presence of Adverse Pressure Gradients

    M. S. Rao / H. A. Hassan | AIAA | 1998

    Generalized matrix force and displacement methods of linear structural analysis

    HUSAIN, H. M. / YETTRAM, A. L. | AIAA | 1965

    A dynamic model for aircraft poststall departure

    HREHA, M. A. / LUTZE, F. H. | AIAA | 1984

    Hypersonic shock-tunnel testing at an equilibrium interface condition of 4100 K

    MINUCCI, M. A. S. / NAGAMATSU, H. T. | AIAA | 1993

    Linear analysis of forced longitudinal waves in rocket motor chambers

    MICCI, M. M. / CAVENY, L. H. / SIRIGNANO, W. A. | AIAA | 1981

    One-equation turbulence model for transonic airfoil flows

    MITCHELTREE, R. A. / HASSAN, H. A. / SALAS, M. D. | AIAA | 1990

    Unsteady vortical disturbances around a thin airfoil in the presenceof a wall

    GEBERT, G. A. / ATASSI, H. M. | AIAA | 1989

    Effects of Mixing Schemes on Kerosene Combustion in a Supersonic Airstream

    M. Owens / C. Segal / A. H. Auslender | AIAA | 1997

    Heat transfer in the entrance region of semicircular ducts with internal fins

    ZHANG, H. Y. / EBADIAN, M. A. | AIAA | 1992

    Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity

    DINYAVARI, M. A. H. / FRIEDMANN, P. P. | AIAA | 1986

    Aeroelastic tailoring - Theory, practice, and promise

    SHIRK, M. H. / HERTZ, T. J. / WEISSHAAR, T. A. | AIAA | 1986

    Experimental and analytical investigation of jets exhausting into a deflecting stream

    MCMAHON, H. M. / MOSHER, D. K. / WRIGHT, M. A. | AIAA | 1970

    Suppression of vortex asymmetry and side force on a circular cone

    Asghar, A. / Stahl, W. H. / Mahmood, M. | AIAA | 1994

    Laboratory study of the charging of spacecraft materials

    LEUNG, M. S. / KAN, H. K. A. | AIAA | 1981

    Stress concentration in the plastic range

    SHERBOURNE, A. N. / HAYDL, H. M. | AIAA | 1976

    Linear analysis of poststall gyrations

    HREHA, M. A. / LUTZE, F. H. | AIAA | 1980

    Characterization of the Pressure Fluctuations Under a Fully Developed Turbulent Boundary Layer

    S. P. Gravante / A. M. Naguib / C. E. Wark et al. | AIAA | 1998

    Toward a Flame Embedding Model for Turbulent Combustion Simulation

    Y. M. Marzouk / A. F. Ghoniem / H. N. Najm | AIAA | 2003

    Experimental study of a two-dimensional scramjet inset, M(freestream) = 10.1-25.1

    MINUCCI, M. A. S. / NAGAMATSU, H. T. | AIAA | 1992

    A study of compressible turbulent reattaching free shear layers

    SAMIMY, M. / PETRIE, H. L. / ADDY, A. L. | AIAA | 1986

    Investigation of a two-dimensional scramjet inlet, freestream M = 8-18 and T0 = 4100 K

    MINUCCI, M. A. S. / NAGAMATSU, H. T. | AIAA | 1993

    F-5E departure warning system algorithm development and validation

    TAYLOR, J. H. / SKOW, A. M. | AIAA | 1988

    Compressible separated flows

    PETRIE, H. L. / SAMIMY,M. / ADDY, A. L. | AIAA | 1986

    Grid embedding technique using Cartesian grids for Euler solutions

    MICHELTREE, R. A. / HASSAN, H. A. / SALAS, M. D. | AIAA | 1988

    Evaluation of a Locally Homogeneous Flow Model of Spray Evaporation

    A. J. Shearer / H. Tamura / G. M. Faeth | AIAA | 1979

    Active flutter suppression for two-dimensional airfoils

    OHTA, H. / NIKIFORUK, P. N. / GUPTA, M. M. et al. | AIAA | 1989

    DESIGN AND PERFORMANCE OF A NEW MULTI-LANE AVI SYSTEM

    Do, M. A. / Chang, C. H. | Taylor & Francis Verlag | 1993

    Operational planning for general aviation facilities at airports

    BURNS, H. C. / WARSKOW, M. A. | AIAA | 1964

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