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High Mach Number Operation of Accelerator Scramjet Engine
Fast and Robust Computation of Optimal Rotor Designs Using Blade Element Momentum Theory
Surrogate Model Development for Optimized Blended-Wing-Body Aerodynamics
Lessons Learned from Large-Scale Aerospace Structural Testing
Monte Carlo Information-Reuse Approach to Aircraft Conceptual Design Optimization Under Uncertainty
Aircraft Design with Active Load Alleviation and Natural Laminar Flow
Surface Mesh Movement Algorithm for Computer-Aided-Design-Based Aerodynamic Shape Optimization
Optimization Study of an Intercooled Recuperated Aero-Engine
Concurrent Design Optimization of Tether-Net System and Actions for Reliable Space-Debris Capture
Active Global Vibration Control of Helicopter Fuselage
Design of an Airbreathing Second Stage for a Rocket-Scramjet-Rocket Launch Vehicle
Aircraft Design Markup Language for Multidisciplinary Aircraft Design and Analysis
Using Dynamical Systems Concepts in Multidisciplinary Design
New Sizing Methodology and Efficiency Analysis of Satellite’s Electrical Power Subsystem
Chandrayaan-3 Trajectory Design: Injection to Successful Landing
Robust Acoustic Objective Functions and Sensitivities in Adjoint-Based Design Optimizations
Bifurcation-Diagram-Free Postflutter Response Constraint for Design Optimization
New Sensitivity Analysis Methods for Complex Modal Parameters in Asymmetrical Damped System
Intelligent Assembly Time Analysis Using a Digital Knowledge-Based Approach
Multiobjective Formulation for Simultaneous Design and Selection of an Uncertainty Set
Taylor Approximation of Second Degree for Complex Mode in Asymmetrical Damped System
Average Generic Vehicle Method for Fleet-Level Analysis of Noise and Emission Tradeoffs
Flutter Characteristics of a Joined-Wing Unmanned Aerial Vehicle with Variable Dihedral Angles
Summary of the 4th High-Lift Prediction Workshop Hybrid RANS/LES Technology Focus Group
Solar Sailing Q-Law for Planetocentric, Many-Revolution Sail Orbit Transfers
Efficient Data-Driven Off-Design Constraint Modeling for Practical Aerodynamic Shape Optimization
Accuracy Limits on Strapdown Velocity and Position Computations
Parametric Covariance Model for Horizon-Based Optical Navigation
Energy Deposition on Analogous Vehicle Panel: Thermal–Structural Response
On Improving the Noise Reduction Performance of Trailing Edge Serrations by Extension
On the Use of Power-Based Parameters for Blowing Active Flow Control Systems
Multifidelity Prediction Framework with Convolutional Neural Networks Using High-Dimensional Data
Spacecraft Attitude Tracking with Guaranteed Performance Bounds
Methodology for Preliminary Flight Control Actuator Design
Investigation of the Composition and Laminar Flame Speed of Pyrolysis Gases
Prediction of Installed Jet Noise from Wave-Packet Models Tuned with Freejet Data
Adaptive-Mesh Sequential Convex Programming for Space Trajectory Optimization
Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing
Conceptual Design of a Space Power System Based on Combustion of Metals