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Freistrahl
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Active Control of a High Reynolds Number Mach 0.9 Axisymmetric Jet
Active control of a high Reynolds number Mach 0.9 axisymmetric jet
Active flow control on the stingray uninhabited air vehicle: Transient behavior
A diffusive gas jet model in PAM-SAFE for airbag inflation
Aeroacoustic investigation of controlled subsonic single jets
Aerodynamic Effects of a 24-Foot, Multisegmented Telescoping Nose Boom on an F-15B Airplane
Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators
Aerodynamic ground effect: a case study of the integration of CFD and experiments
Aerodynamics of 3-D Aircraft Afterbodies (L'Aerodynamique des Arriere-corps Tridimensionnels)
Aerodynamics of a jet in the vortex wake of a wing
Analysis of Concentric Canister Wall Roughness Effect on Jet Flow Based on Fluid Dynamics
Analytic Calculation of Two-Dimensional Supersonic Jets
A New Support Structure in Waverider Force Measurement
An Experimental Air-Cushion Vehicle PV-1 Summary Report
An experimental investigation of a three-dimensional wall jet
A numerical study of jet entrainment effects on the subsonic flow over nozzle afterbodies
A numerical study on the generation of impulsive noise by complex flows discharging from a muzzle
A preliminary experimental investigation of the flowfield of a planar wall jet
Aspirating pipes do not flutter at infinitesimally small flow
A two-step computational aeroacoustics method applied to high-speed flows
Basic Aerodynamic Research on the Airframe Integration of High Bypass Engines, Part 1
Calculation of an unsteady jet flow around the plate cascade
Cart3D Simulations for the First AIAA Sonic Boom Prediction Workshop
CFD Simulation of Liquid Rocket Engine Injectors. Part 1. Simulations of the RCM-1 Experiments
Comparison of Measured and Predicted Flight Effects on High-Bypass Coaxial Jet Exhaust Noise
Comparison of planar fluorescence measurements and computational modeling of shock-layer flow
Computational Analysis of Forebody Tangential Slot Blowing on the High alpha Research Vehicle
Conceptual Design of a Supersonic Business Jet Propulsion System
Control of flow structure on delta wing with steady trailing-edge blowing