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Wall Heat Loads in a Cryogenic Rocket Thrust Chamber During Thermoacoustic Instabilities
Variable Structure Model for Flow-Induced Tonal Noise Control with Plasma Actuators
Validation of Pulse-Detonation Operation in Low-Ambient-Pressure Environment
Utilization of Nonthermal Plasma in Pulse Detonation Engine Ignition
Unsteady Thrust Measurement for Pulse Detonation Engines
Unexpected Collision Detection, Estimation, and Reaction for a Free-Flying Orbital Robot
Time-Resolved Flowfield Measurements of Momentum-Driven Pulsed Transient Jets
Thrust Characteristics of High-Density Helicon Plasma Using Argon and Xenon Gases
Three-Electrode Plasma Synthetic Jet Actuator for High-Speed Flow Control
Theoretical Model for the Gust Performance of Closed-Loop Flight Control
Theoretical and Experimental Investigations of the Pulse Tube Engine
Temperatures of Spark Kernels Discharging into Quiescent or Crossflow Conditions
Temperature Estimates of Exhaust Plumes from a Turbine Driven by Pulsed Detonations
Starting Process of a Pulsed Jet as Seen by Schlieren Measurements
Smoked Foil on Deflagration-to-Detonation Transition
Simulations and Flight Tests of a New Nonlinear Controller for the EAGLE Lander
Shock Transfer and Shock-Initiated Detonation in a Dual Pulse Detonation Engine/Crossover System
Shock-Initiated Combustion in an Airbreathing, Pulse Detonation Engine-Crossover System
Satellite Formation-Containment Flying Control with Collision Avoidance
Riemann–Stieltjes Optimal Control Problems for Uncertain Dynamic Systems
Reynolds Number Effects on Fully Developed Pulsed Jets Impinging on Flat Surfaces
Real-Time Closed-Loop System Identification of a Quadcopter
Radar Terminal Descent Sensor Performance During Mars Science Laboratory Landing
Quaternion-Based Bang-Bang Attitude Stabilizer for Rotating Rigid Bodies
Pulsed Jets Laminar Separation Control Using Instability Exploitation
Optimal Midcourse Guidance for Dual-Pulse Rocket Using Pseudospectral Sequential Convex Programming
One Method to Increase the Operating Frequency of Pulse Detonation Rocket Engines
Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure
Non-Premixed Burner-Attached Jet Flames in Crossflow Pulsed at Resonance Frequency
Neutral Gas Expansion in a Cylindrical Helicon Discharge Chamber
Near-Optimal Feedback Strategies Synthesized Using a Spatial Statistical Approach
Mitigating Time-Delay in Nonlinear Dynamics Inversion for Multirotor Unmanned Aerial Vehicles
Minimum-Eigenvalue-Based Fault-Tolerant Adaptive Dynamic Control for Spacecraft
Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles
Low-Cost Laser Range-Measurement-Based Terrain-Following Concept and Error Analysis
Large Low-Frequency Oscillations Initiated by Flow Control on a Poststall Airfoil
to Mars: A Combined Robotic/Piloted Mars Mission
Investigating the Chemical Stability of Electrospray Plumes During Particle Collisions
Interaction Behavior of Pulsejet Engines
Integrated Optimization for Single-Stage-to-Orbit Using a Pulse Detonation Engine
Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster
High-Frequency Pulsed Combustion Actuator Experiments