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Flugmechanik
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Development of Advanced High Lift Leading Edge Technology for Laminar Flow Wings
Flow Quality Surveys in the Settling Chamber of the NASA Glenn Icing Research Tunnel (2011 Tests)
Improved Aerodynamic Analysis for Hybrid Wing Body Conceptual Design Optimization
An Exploratory Investigation of a Slotted, Natural-Laminar-Flow Airfoil
DRE-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers
Supersonic Aerodynamic Characteristics of Blunt Body Trim Tab Configurations
Display Provides Pilots with Real-Time Sonic-Boom Information
Numerical Investigation of a Fuselage Boundary Layer Ingestion Propulsion Concept
Airloads Correlation of the UH-60A Rotor Inside the 40- by 80-Foot Wind Tunnel
High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept
Nonlinear Flight Dynamics of Very Flexible Aircraft
Mars Entry Instrumentation Flight Data and Mars 2020 Entry Environments
Untersuchungen zu Energieversorgung und Antrieb einer Leichter-als-Luft-Höhenplattform
Computational Analysis of a Multiple-Nozzle Supersonic Retropropulsion Configuration
2001 Flight Mechanics Symposium
High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept
Experimental Sonic Boom Measurements on a Mach 1.6 Cruise Low-Boom Configuration
Modeling and Simulation of Rotary Sloshing in Launch Vehicles
Guidance, Flight Mechanics and Trajectory Optimization. Volume 3 - the Two-Body Problem
Sensitivity of the Asteroid Redirect Robotic Mission (ARRM) to Launch Date and Asteroid Stay Time
Experimental Investigation of a Large-Scale Low-Boom Inlet Concept
Reynolds-Averaged Navier-Stokes Simulation of a 2D Circulation Control Wind Tunnel Experiment
Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
Structural Implementations of Leading-Edge Noise Reduction Devices
Analysis of Near Rectilinear Halo Orbit Insertion with a 40-kW Solar Electric Propulsion System
Analysis of Near Rectilinear Halo Orbit Insertion with a 40-kW Solar Electric Propulsion System
The Effects of Ambient Conditions on Helicopter Harmonic Noise Radiation: Theory and Experiment
Trajectory Design for a Single-String Impactor Concept
Blade Displacement Measurements of the Full-Scale UH-60A Airloads Rotor