Synonyms were used for:
Analysis
•
numerische Analysis
Search without synonyms:
keywords:(numerische Analysis)
Genetic Algorithm Optimization of a Cost Competitive Hybrid Rocket Booster
Georegistration of Earth Observing-1 (EO-1) Data Using Global Land Survey (GLS) Maps
Global transformation of rotation matrices to Euler parameters
Grid resolution and solution convergence for Mars Pathfinder forebody
Head Pose Estimation Using Multilinear Subspace Analysis for Robot Human Awareness
High-Fidelity Analysis of Lift+Cruise VTOL Urban Air Mobility Concept Aircraft
High-Fidelity CFD Verification Workshop 2024: Spalart-Allmaras QCR2000-R Turbulence Model
High-Fidelity CFD Verification Workshop 2024: Spalart-Allmaras QCR2000-R Turbulence Model
High-Fidelity Simulations of Lift+Cruise VTOL Urban Air Mobility Concept Aircraft in Hover
High-Fidelity Simulations of Lift+Cruise VTOL Urban Air Mobility Concept Aircraft in Hover
High Speed Solution of Spacecraft Trajectory Problems Using Taylor Series Integration
Impact of Analytic Derivatives on Optimization of N-Impulse Orbit Transfer
Improved Convergence and Robustness of USM3D Solutions on Mixed-Element Grids
Improved Convergence and Robustness of USM3D Solutions on Mixed-Element Grids
Improved flux-split algorithm applied to hypersonic flows in chemical equilibrium
Improved solution for ill-conditioned algebraic equations by epsilon decomposition
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP)
Institute for Computational Mechanics in Propulsion (ICOMP) fourth annual review, 1989
Inverse Estimation of Mars 2020 Entry Aeroheating Environments Using MEDLI2 Flight Data
Iteration strategy for upwind/relaxation solutions to the thin-layer Navier-Stokes equations
Jig-Shape Optimization of a Low-Boom Supersonic Aircraft
Jig-Shape Optimization of Quiet Supersonic Technology X-Plane
Krylov model reduction algorithm for undamped structural dynamics systems
Launch, Ascent, and Vehicle Aerodynamics Scale-Resolving Simulations for NASA Applications
Least-Squares Adaptive Control Using Chebyshev Orthogonal Polynomials
Level-Set Topology Optimization with Aeroelastic Constraints
Linear and Geometrically Nonlinear Structural Shape Sensing from Strain Data
LPV Modeling of a Flexible Wing Aircraft Using Modal Alignment and Adaptive Gridding Methods
Modeling Meteoroid Densities for Spacecraft Risk Assessment
Modeling of Gaseous Oxygen Liquefaction Inside Mars Ascent Vehicle Propellant Tank