Wind Tunnel Investigation of an Oblique Wing Transport Model at Mach Numbers Between 0.6 and 1.4
Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Airplane
Wind-Tunnel Investigation of a Flush Airdata System at Mach Numbers from 0.7 to 1.4
Wind-Tunnel Investigation of Actuated Forebody Strakes for Yaw Control at High Angles of Attack
Wind-Tunnel Investigation of a 4-Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing
Wind-Tunnel Free-Flight Investigation of a Supersonic Persistence Fighter
Wind-Tunnel Free-Flight Investigation of a 0.15-Scale Model of the F-106B Airplane with Vortex Flaps
Wind Tunnel Evaluation of a Truncated NACA 64-621 Airfoil for Wind Turbine Applications
Wind-Tunnel Evaluation of a 21-Percent-Scale Powered Model of a Prototype Advanced Scout Helicopter
Wind-Tunnel Evaluation of a 21 Percent-Scale Powered Model of a Prototype Advanced Scout Helicopter
Wind Tunnel and Flight Test Stability and Control Derivatives for the X-24A Lifting Body
Wind Tunnel and Flight Evaluation Rosemount Shielded Pitot-Static Tube Model 850N
Wind Tunnel Analysis And Flight Test of A Wing Fence On A T-38