61–80 of 161 hits
|

    Modeling Hubble Space Telescope flight data by Q-Markov cover identification

    Liu, K. / Skelton, R. E. / Sharkey, J. P. | AIAA | 1994

    Downstream Mixing Gasdynamic Lasers-A Numerical Solution

    K. N. ParthaSarathy / J. D. Anderson E. Jones | AIAA | 1979

    Simulation evaluation of an advanced control concept for a V/STOL aircraft

    MORALEZ, E. / MERRICK, V. K. / SCHROEDER, J. A. | AIAA | 1989

    Solar simulation testing of the nuclear test detection spacecraft.

    GLENN, E. E. / GOLDMAN, K. L. / LEHR, S. N. et al. | AIAA | 1966

    Structural similarity of turbulence in fully developed smooth pipe flow

    LAI, J. C. S. / BULLOCK, K. J. / KRONAUER, R. E. | AIAA | 1989

    A new relative referencing method for crop monitoring using chlorophyll fluorescence

    Norikane, J. / Goto, E. / Kurata, K. et al. | Elsevier | 2002

    Performance Cycle Analysis of Turbofan Engine with Interstage Turbine Burner

    K. H. Liew / E. Urip / S. L. Yang et al. | AIAA | 2006

    Orbit determination using analytic partial derivatives of perturbed motion

    ARSENAULT, J. L. / FORD, K. C. / KOSKELA, P. E. | AIAA | 1970

    Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program

    O. A. Powell / J. T. Edwards / R. B. Norris et al. | AIAA | 2001

    Supersonic Dynamic Stability Experiments on the Space Shuttle

    K. J. ORLIK-RUCKEMANN / J. G. LABERGE AND E. S. HANFF | AIAA | 1972

    Discontinuous wing leading edge to enhance spin resistance

    DICARLO, D. J. / GLOVER, K. E. / STEWART, E. C. et al. | AIAA | 1985

    Performance degradation of a model helicopter rotor with a generic ice shape

    KORKAN, K. D. / CROSS, E. J. / MILLER, T. L. | AIAA | 1984

    Optimal estimation of rotation-coupled flexural oscillations

    FARRELL, J. L. / MILLER, J. A. / NEWTON, J. K. et al. | AIAA | 1969

    Classical and neo-classical cruise-dash optimization

    BILIMORIA, K. D. / CLIFF, E. M. / KELLEY, H. J. | AIAA | 1985

    Spectrally Resolved Measurement of Flame Radiation to Determine Soot Temperature and Concentration

    D. R. Snelling / K. A. Thomson / G. J. Smallwood et al. | AIAA | 2002

    Numerical evaluation of propeller noise including nonlinear effects

    KORKAN, K. D. / VON LAVANTE / E. et al. | AIAA | 1986

    Validation of an Experimentally Derived Uncertainty Model

    K. B. Lim / D. E. Cox / G. J. Balas et al. | AIAA | 1998

    Design and operation of a supersonic annular flow facility

    Williams, K. E. / Gessner, F. B. / Harloff, G. J. | AIAA | 1994

    Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated ice

    KORKAN, K. D. / CROSS, E. J. / CORNELL, C. C. | AIAA | 1985

    Depriming/rewetting of arterial heat pipes - Comparison with Share-II flight experiment

    Ochterbeck, J. M. / Peterson, G. P. / Ungar, E. K. | AIAA | 1995