41 |
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AIAA journal
중앙도서관 대출불가(별치)
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American Institute of Aeronautics and Astronautics
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American Institute of Aeronautics and Astronautics
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1963-
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42 |
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Aileron Buzz Simulation Using an Implicit Multiblock Aeroelastic Solver/
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Yang, G
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American Institute of Aeronautics and Astronautics
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2003
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43 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Active and Passive Suppressions of Nonlinear Panel Flutter Using Finite Element Method/
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Moon, S H
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American Institute of Aeronautics and Astronautics
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2001
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44 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators/
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Amitay, M
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American Institute of Aeronautics and Astronautics
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2001
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45 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Aerodynamic Optimization of Supersonic Transport Wing Using Unstructured Adjoint Method/
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Kim, H-J
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American Institute of Aeronautics and Astronautics
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2001
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46 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Aerodynamics of Gurney Flaps on a Wing in Ground Effect/
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Zerihan, J
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American Institute of Aeronautics and Astronautics
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2001
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47 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Characterization and Analysis of Magnetorheological Damper Behavior Under Sinusoidal Loading/
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Snyder, R A
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American Institute of Aeronautics and Astronautics
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2001
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48 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Compressible Dynamic Stall Control Using Dynamic Shape Adaptation (TN)/
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Chandrasekhara, M S
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American Institute of Aeronautics and Astronautics
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2001
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49 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Computational Aeroacoustic Analysis of Slat Trailing-Edge Flow/
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Singer, B A
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American Institute of Aeronautics and Astronautics
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2000
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50 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Computation of Mistuning Effects on Cascade Flutter/
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Sadeghi, M
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American Institute of Aeronautics and Astronautics
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2001
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51 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Convergence Acceleration of an Inverse Design Technique for Constructing Turbomachinery Cascades (TN)/
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Yokota, J W
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American Institute of Aeronautics and Astronautics
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2000
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52 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Coupled Analytical Sensitivity Analysis and Optimization of Three-Dimensional Nonlinear Aeroelastic Systems/
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Maute, K
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American Institute of Aeronautics and Astronautics
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2001
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53 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Coupled Helicopter Rotor/Flexible Fuselage Aeroelastic Model for Control of Structural Response/
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Cribbs, R C
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American Institute of Aeronautics and Astronautics
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2000
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54 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Damping Perturbation Method for Flutter Solution: The g-Method/
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Chen, P C
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American Institute of Aeronautics and Astronautics
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2000
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55 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Detection and Repair of Poorly Converged Optimization Runs/
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Kim, H
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American Institute of Aeronautics and Astronautics
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2001
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56 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Diffusion Timescale of Porous Pressure-Sensitive Paint (TN)/
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Liu, T
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American Institute of Aeronautics and Astronautics
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2001
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57 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Double Flutter in an Aeroelastic System (TN)/
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Chamara, R A
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American Institute of Aeronautics and Astronautics
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2001
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58 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effect of Ribs on Suddenly Expanded Flows (TN)/
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Rathakrishnan, E
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American Institute of Aeronautics and Astronautics
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2001
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59 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effect of Wall Shear Stress on Structural Vibration (TN)/
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Frendi, A
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American Institute of Aeronautics and Astronautics
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2001
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60 |
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing/
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Tang, D
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American Institute of Aeronautics and Astronautics
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2001
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