1–50 von 161 Ergebnissen
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    2001 Mars Odyssey Orbit Determination During Interplanetary Cruise

    P. G. Antreasian / D. T. Baird / J. S. Border et al. | AIAA | 2005

    A comprehensive model for AP-based composite propellant ignition

    KUMAR, M. / WILLS, J. E. / KULKARNI, A. K. et al. | AIAA | 1984

    Acoustic-vortex interactions and low-frequency oscillations in axisymmetric combustors

    KAILASANATH, K. / GARDNER, J. H. / BORIS, J. P. et al. | AIAA | 1989

    Aerodynamic side force induced by nozzle entrance flow asymmetry

    VARWIG, R. L. / WHITTIER, J. S. / DURRAN, D. A. et al. | AIAA | 1989

    Aeroelastic design optimization program

    DODD, A. J. / KADRINKA, K. E. / LOIKKANEN, M. J. et al. | AIAA | 1990

    A Laser System to Measure Rocket Attitude in Flight

    K. M. Pell / J. E. Nydahl / R. G. Conard et al. | AIAA | 1978

    A new relative referencing method for crop monitoring using chlorophyll fluorescence

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

    An existing facility for scramjet testing - The wave superheater.

    CARPENTER, J. E. / GRAVES, K. W. | AIAA | 1967

    Application of Encke's method to long arc orbit determination solutions

    LUNDBERG, J. B. / SCHUTZ, B. E. / FIELDS, R. K. et al. | AIAA | 1991

    A Relaxation Solution of Transonic Nozzle Flows Including Rotational Flow Effects

    E. F. Brown / T. J. F. Brechtt / K. E. Walsh | AIAA | 1977

    A translog cost model of the bulk shipping industry

    Tolofari, S. R. / Button, K. J. / Pitfield, D. E. | Taylor & Francis Verlag | 1987

    BBXRT observations of supernova remnants

    Petre, R. / Serlemitsos, P. / Marshall, F. et al. | Elsevier | 1993

    Book reviews

    Rogers, K. G. / Weaver, T. E. / Maher, M. et al. | Taylor & Francis Verlag | 1972

    Boundary-layer development on moving walls using an integral theory

    FANSLER, K. S. / DANBERG, J. E. | AIAA | 1976

    Boundary-layer separation on moving walls using an integral theory

    FANSLER, K. S. / DANBERG, J. E. | AIAA | 1977

    Characterization of large-scale structures in a forced ducted flow with dump

    SCHADOW, K. C. / WILSON, K. J. / GUTMARK, E. | AIAA | 1987

    Classical and neo-classical cruise-dash optimization

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

    Codag — dust agglomeration experiment in micro-gravity

    Keller, H.U. / Blum, J. / Donn, B. et al. | Elsevier | 1993

    Combustion enhancement by axial vortices

    GUTMARK, E. / SCHADOW, K. C. / PARR, T. P. et al. | AIAA | 1989

    Combustion of ammonium perchlorate-polymer sandwiches

    PRICE, E. W. / HANDLEY, J. C. / PANYAM, R. R. et al. | AIAA | 1981

    Combustion-related shear-flow dynamics in elliptic supersonic jets

    SCHADOW, K. C. / GUTMARK, E. / KOSHIGOE, S. et al. | AIAA | 1989

    Comet Halley: Nucleus and jets (results of the VEGA mission)

    Sagdeev, R.Z. / Avanesov, G.A. / Barinov, I.V. et al. | Elsevier | 1985

    Comet plasma tail formation — Giotto observations

    Wilken, B. / Jockers, K. / Johnstone, A.D. et al. | Elsevier | 1986

    Comet simulation experiments in the DFVLR space simulators

    Kochan, H. / Feuerbacher, B. / Joo, F. et al. | Elsevier | 1989

    Comment on "X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data"

    Dinesh K. Prabhu / Joseph G. Marvin / Carol B. Davies et al. | AIAA | 2003

    Comparison of Measurements and Predictions for Blowing from a Turbine Blade Tip

    E. Couch / J. Christophel / E. Hohlfeld et al. | AIAA | 2005

    Comprehensive analysis of two downburst-related aircraft accidents

    Shen, J. / Parks, E. K. / Bach, R. E. | AIAA | 1996

    Compressive Response of Lightweight Ceramic Ablators: Phenolic Impregnated Carbon Ablator

    Kelly E. Parmenter / Karl Shuman / Frederick Milstein et al. | AIAA | 2001

    Compressive Response of Lightweight Ceramic Ablators: Silicone Impregnated Reusable Ceramic Ablator

    Kelly E. Parmenter / Karl Shuman / Frederick Milstein et al. | AIAA | 2002

    Computational Investigation of Three-Dimensional Flow Effects on Micronozzles

    R. D. D. Menzies / B. E. Richards / K. J. Badcock et al. | AIAA | 2002

    Computational study of viscous effects on lobed mixer flow features and performance

    O'Sullivan, M. N. / Krasnodebski, J. K. / Waitz, I. A. et al. | AIAA | 1996

    Computational Treatment of Source Terms in Two-Equation Turbulence Models

    B. Merci / J. Steelant / J. Vierendeels et al. | AIAA | 2000

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

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

    Design and operation of a supersonic annular flow facility

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

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

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

    Discontinuous wing leading edge to enhance spin resistance

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

    Downstream Mixing Gasdynamic Lasers-A Numerical Solution

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

    Downwash for joined-wing airframe with control surface deflections

    BURKHALTER, JOHN E. / SPRING, DONALD J. / KEY, M. K. | AIAA | 1992

    Effects of Periodic Atomization on Combustion Instability in Liquid-Fueled Propulsion Systems

    W. E. Anderson / K. L. Miller / H. M. Ryan et al. | AIAA | 1998

    Electric power from vertical-axis wind turbines

    TOURYAN, K. J. / Moriah Research Co. / Denver et al. | AIAA | 1987