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Flugmechanik
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THE INCREASING PROMINENCE OF THE ENGINEERING TECHNICIAN IN NASA
Aerodynamic Spring and Damping of Free-Pitching Tips on a Semispan Wing
Analytical solutions to constrained hypersonic flight trajectories
Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
Aerodynamic Properties Analysis of Rapid Prototyped Models Versus Conventional Machined Models
A High Altitude-Low Reynolds Number Aerodynamic Flight Experiment
Hyper-X Research Vehicle (HXRV) Experimental Aerodynamics Test Program Overview
Hyper-X Research Vehicle (HXRV) Experimental Aerodynamics Test Program Overview
An Overview of Unsteady Pressure Measurements in the Transonic Dynamics Tunnel
Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments
Aeroelastic Deformation Measurements of Flap, Gap, and Overhang on a Semispan Model
Contributions of the Langley Transonic Dynamics Tunnel to Rotorcraft Technology and Development
Effects of Passive Porosity on Interacting Vortex Flows At Supersonic Speeds
Contributions of Transonic Dynamics Tunnel Testing to Airplane Flutter Clearance
Evaluation of Airfoil Dynamic Stall Characteristics for Maneuverability
Aerothermodynamic Analysis of the Project FIRE II Afterbody Flow
Computation of External Aerodynamics for a Canard Rotor/Wing Aircraft
Hyper-X Engine Testing in the NASA Langley 8-Foot High Temperature Tunnel
Research on the F/A-18E/F Using a 22%-Dynamically-Scaled Drop Model
Aeroelastic Response of Swept Aircraft Wings in a Compressible Flow Field
Summary of Transition Results From the F-16XL-2 Supersonic Laminar Flow Control Experiment
Aerodynamic Characteristics, Database Development and Flight Simulation of the X-34 Vehicle
Reynolds Number Effects on a Supersonic Transport at Transonic Conditions
Forebody Aerodynamics of the F-18 High Alpha Research Vehicle with Actuated Forebody Strakes
A Rapid Aerodynamic Design Procedure Based on Artificial Neural Networks
Parameter Sensitivity Study of the Wall Interference Correction System (WICS)
Prediction of Unsteady Aerodynamic Coefficients at High Angles of Attack