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제한항목: American Institute of Aeronautics and Astronautics

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검색리스트 테이블
No	서명	저자	발행처	원문제공시작년
21	Improved Turbulent Boundary-Layer Model for Shock Tubes/	Petersen, E. L	American Institute of Aeronautics and Astronautics	1900

22	Improvement in Model Reduction Schemes Using the System Equivalent Reduction Expansion Process	Papadopoulos, M	American Institute of Aeronautics and Astronautics	1996

23	Improvement of Explicit Multistage Schemes for Central Spatial Discretization (TN)	Tai, C.-H	American Institute of Aeronautics and Astronautics	1996

24	Improvements to a Dual-Time-Stepping Method for Computing Unsteady Flows(TN)	DeRango, S	American Institute of Aeronautics and Astronautics	1997

25	Improving Curved Subsonic Diffuser Performance with Vortex Generators	Reichert, B. A	American Institute of Aeronautics and Astronautics	1996

26	Impulsively Started Turbulent Jets	Johari, H	American Institute of Aeronautics and Astronautics	1997

27	Impulsive Start of a Symmetric Airfoil at High Angle of Attack	Katz, J	American Institute of Aeronautics and Astronautics	1996

28	Inclusion of Transverse Shear Deformation In Optimum Design of Aircraft Wing Panels	Williams, P. W. L	American Institute of Aeronautics and Astronautics	1996

29	Incompressible Flow, Second Edition	Knight, D	American Institute of Aeronautics and Astronautics	1996

30	Incremental Potential Flow Based Membrane Wing Element	Smith, R	American Institute of Aeronautics and Astronautics	1997

31	Infeasible Path Optimal Design Methods with Applications to Aerodynamic Shape Optimization	Orozco, C. E	American Institute of Aeronautics and Astronautics	1996

32	In-Flight Imaging of Transverse Gas Jets Injected into Compressible Crossflows	Wang, K. C	American Institute of Aeronautics and Astronautics	1995

33	Inflow Boundary Conditions for Hybrid Large Eddy/Reynolds Averaged Navier-Stokes Simulations/	Xiao, X	American Institute of Aeronautics and Astronautics	2003

34	Influence of Contact Phenomena on Embedded Delaminations Growth in Composites/	Riccio, A	American Institute of Aeronautics and Astronautics	2003

35	Influence of Elastomeric Damper Modeling on the Dynamic Response of Helicopter Rotors	Kunz, D. L	American Institute of Aeronautics and Astronautics	1997

36	Influence of Film Cooling on the Secondary Flow in a Turbine Nozzle	Langowsky, C	American Institute of Aeronautics and Astronautics	1997

37	Influence of Four Kinds of Gradient Magnetic Fields on Hydrogen-Oxygen Flame/	Yamada, E	American Institute of Aeronautics and Astronautics	2003

38	Influence of Surface Flow on Aerodynamic Loads of a Cantilever Wing	Huang, R. E	American Institute of Aeronautics and Astronautics	1996

39	Influence of Turbulence Modeling on Predictions of Turbulent Combustion	Gran, I. R	American Institute of Aeronautics and Astronautics	1997

40	Influences of Blade Bowing on Flowfields of Turbine Stator Cascades/	Tan, C	American Institute of Aeronautics and Astronautics	2003

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