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Absaugen
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Experiments with a Wing Model from which the Boundary Is Removed by Suction
Device for Sucking Air from an Aerodynamic Surface
Experiments with an Airfoil from which the Boundary Layer Is Removed by Suction
Research on High Lift Boundary Layer Suction Investigations on Thin High Speed Wings
Research on High Lift Boundary Layer Suction Investigations on Thin High Speed Wings
Determination of the Velocity Field of an Airfoil with Leading Edge Suction
Boundary Layer Control by Porous Area Suction on the Wing Leading Edges of an F-86F Airplane
Research on High Lift Boundary Layer Suction Investigations on Thin High Speed Wings
Circulation Control by Slot Suction on a Circular Cylinder - Preliminary Measured Force Data
Tests of the Bell Aerospace LA-4 ACLS Fitted with Suction Braking and Predictions for Other Aircraft
Self-Contained Backflush/Start System for Suction LFC Undersea Vehicle
Self-Contained Backflush/Start System for Suction LFC Undersea Vehicle
Aircraft Design Studies - Counter Insurgency Aircraft with Suction Boundary Layer Control
Investigation on the Cooling of Exhaust Gas by Direct Contact Between Exhaust Gas and Water
Conceptual Design Study of Air Bearing/Suction Hold-Down Devices for Vertical Landing Aircraft
Selected Scientific and Technical Contributions of Edward C. Polhamus
Unsteady Pressure Field and Vorticity Productiion at the Suction Surface of a Pitching Airfoil
Forebody Flow Visualization on the F-18 HARV with Actuated Forebody Strakes
Analysis and Experimental Verification of Axial Thrust on the M-1 Liquid Oxygen Turbopump
Tests of the NACA 65 sub 3 -018 Airfoil Section with Boundary-Layer control by Suction
Evaluation of Laminar Flow Control System Concepts for Subsonic Commercial Transport Aircraft
Evaluation of Viscous Drag Reduction Schemes for Subsonic Transports
Climbing Crawling Robot (A Unique Cable Robot for Space and Earth)
High Reynolds Number Hybrid Laminar Flow Control (HLFC) Flight Experiment, Report 2
Wind Tunnel Tests of 16 Percent Thick Airfoil Section with Spoilers at Different Chordwise Positions
Study of Supersonic Wings Employing the Attainable Leading-Edge Thrust Concept