Enhancing Model Predictability for a Scramjet Using Probabilistic Learning on Manifolds
来源期刊:AIAA JournalDOI:10.2514/1.J057069
Enriched Piston Theory for Expedient Aeroelastic Loads Prediction in the Presence of Shock Impingements
来源期刊:AIAA JournalDOI:10.2514/1.J057595
Machine-Learning-Based Detection of Aerodynamic Disturbances Using Surface Pressure Measurements
来源期刊:AIAA JournalDOI:10.2514/1.j058486
Active Flow Control Virtual Maneuvering System Applied to Conventional Airfoil
来源期刊:AIAA JournalDOI:10.2514/1.J056258
Computation of Hypersonic Flows over Flying Configurations Using a Nonlinear Constitutive Model
来源期刊:AIAA JournalDOI:10.2514/1.J057688
Experimental study of swept impinging oblique shock boundary layer interaction
来源期刊:AIAA JournalDOI:10.2514/6.2019-0340
Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs
来源期刊:AIAA JournalDOI:10.2514/1.J057892
Attenuation of Flow Separation Using Herringbone Riblets at M∞=5
来源期刊:AIAA JournalDOI:10.2514/1.J057215
Lamination Parameter Interpolation Method for Design of Manufacturable Variable-Stiffness Composite Panels
来源期刊:AIAA JournalDOI:10.2514/1.J057902
Experimental Investigations of Film Cooling in a Conical Nozzle Under Rocket-Engine-Like Flow Conditions
来源期刊:AIAA JournalDOI:10.2514/1.J057486
Exergetic Drag Characteristic Curves
来源期刊:AIAA JournalDOI:10.2514/1.J057985
Shape Optimization Using the Adjoint Lattice Boltzmann Method for Aerodynamic Applications
来源期刊:AIAA JournalDOI:10.2514/1.J057955
Effect of Forcing on a Supersonic Compression Ramp Flow
来源期刊:AIAA JournalDOI:10.2514/1.J058504
Computationally Efficient Concurrent Multiscale Framework for the Nonlinear Analysis of Composite Structures
来源期刊:AIAA JournalDOI:10.2514/1.J057880
Active Separation Control at the Pylon-Wing Junction of a Real-Scale Model
来源期刊:AIAA JournalDOI:10.2514/1.J057345
Energy-Based Drag Breakdown in Compressible Flow by Wake-Plane Integrals
来源期刊:AIAA JournalDOI:10.2514/1.J058114
Three-Component Turbulence Measurements and Analysis of a Supersonic, Axisymmetric Base Flow
来源期刊:AIAA JournalDOI:10.2514/1.J057859
Quantitative Features of Wingtip Vortex Wandering Based on the Linear Stability Analysis
来源期刊:AIAA JournalDOI:10.2514/1.J057693
Aeroelastic Stability Analysis of Tailored Pretwisted Wings
来源期刊:AIAA JournalDOI:10.2514/1.j058575
Active Polynomial Chaos Expansion for Reliability-Based Design Optimization
来源期刊:AIAA JournalDOI:10.2514/1.J058020
Computational Analysis of Interaction of a Sweeping Jet with an Attached Crossflow
来源期刊:AIAA JournalDOI:10.2514/1.J057191
Efficient Aeroelastic Solution Based on Time-Spectral Fluid–Structure Interaction Method
来源期刊:AIAA JournalDOI:10.2514/1.J057628
Frequency Control of Thin Plates with Light-Activated Shape-Memory Polymers
来源期刊:AIAA JournalDOI:10.2514/1.J058273
Topology Optimization of Solid Rocket Fuel
来源期刊:AIAA JournalDOI:10.2514/1.J057807
Shock Control of a Low-Sweep Transonic Laminar Flow Wing
来源期刊:AIAA JournalDOI:10.2514/1.J058011
Application of Resonant Femtosecond Tagging Velocimetry in the 0.3-Meter Transonic Cryogenic Tunnel
来源期刊:AIAA JournalDOI:10.2514/1.J057981
Quality-Preserving Linear Elasticity Mesh Movement Algorithm for Multi-Element Unstructured Meshes
来源期刊:AIAA JournalDOI:10.2514/1.J057463
Beam Theory for Asymptotic Analysis of Aperiodic and Inhomogeneous Structures
来源期刊:AIAA JournalDOI:10.2514/1.J057563
Iterative Component Mode Synthesis Using a Priori and a Posteriori Criteria
来源期刊:AIAA JournalDOI:10.2514/1.J057661
Mode Behavior in Supersonic Cavity Flows
来源期刊:AIAA JournalDOI:10.2514/1.J057818
Enhanced Stability of Two-Material Panels in Supersonic Flow: Optimization Strategy and Physical Explanation
来源期刊:AIAA JournalDOI:10.2514/1.j057965
Review of Laminated Composite Plate Theories, with Emphasis on Variational Asymptotic Method
来源期刊:AIAA JournalDOI:10.2514/1.J057552
Mutual Effect Between Swept-and-Leaned Vanes and Acoustic Liners on Fan Interaction-Noise Reduction
来源期刊:AIAA JournalDOI:10.2514/1.J057854
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Large-Scale Hypersonic Facility
来源期刊:AIAA JournalDOI:10.2514/1.J057759
Estimation of Inflow Uncertainties in Laminar Hypersonic Double-Cone Experiments
来源期刊:AIAA JournalDOI:10.2514/1.J059033
Multifield Variational Sectional Analysis for Accurate Stress Computation of Multilayered Composite Beams
来源期刊:AIAA JournalDOI:10.2514/1.J057384
Local Stochastic Vortex Structure Method for Synthetic Turbulence Computation in Flight Simulators
来源期刊:AIAA JournalDOI:10.2514/1.J057329
U.S. Army Rotorcraft Research at Ames: New Frontier in Dynamics and Aeroelasticity
来源期刊:AIAA JournalDOI:10.2514/1.J057503
Acoustic Excitation as Triggering Mechanism of the “DC Shift” in Hybrid Rockets
来源期刊:AIAA JournalDOI:10.2514/1.j058139
Effect of Nonequilibrium Reacting Flow on Flutter at Hypersonic Flight Speed
来源期刊:AIAA JournalDOI:10.2514/1.J057713
Validation of the Steady-State Hover Formulation for Accurate Performance Predictions
来源期刊:AIAA JournalDOI:10.2514/1.j058408
Performance Characteristics of Airfoils with Leading-Edge Tubercles and an Internal Slot
来源期刊:AIAA JournalDOI:10.2514/1.J058145
Aerodynamic Parameter Prediction via Artificial Hair Sensors with Signal Power in Turbulent Flow
来源期刊:AIAA JournalDOI:10.2514/1.J057632
Effect of Geometric Configurations on the Starting Transients in Vacuum Ejector
来源期刊:AIAA JournalDOI:10.2514/1.J058071
Structure-Based Model of a Forced Shear Layer
来源期刊:AIAA JournalDOI:10.2514/1.J057422
Effects of Perforated Liners on Controlling Combustion Instabilities in Annular Combustors
来源期刊:AIAA JournalDOI:10.2514/1.J059099
Verification of Unstructured Grid Adaptation Components
来源期刊:AIAA JournalDOI:10.2514/1.j058783
Nonlinear Modal Interactions of Swept Composite Aircraft Wings Carrying External Stores
来源期刊:AIAA JournalDOI:10.2514/1.J057582
Onset of Transient Shock Interaction with Cavity Shear Layer
来源期刊:AIAA JournalDOI:10.2514/1.J058448
Stability Analysis of the Swirling Majdalani–Fist Mean Flowfield in Solid Rocket Motors
来源期刊:AIAA JournalDOI:10.2514/1.j058568