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LIFT
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XH-59A ABC Technology Demonstrator Altitude Expansion and Operational Tests
X-19 V/STOL Technology: A Critical Review (Final Report)
Wind-tunnel Tests of a Wing with a Trailing-edge Auxiliary Airfoil Used as a Flap
Wind-Tunnel Tests of a Series of Parachutes Designed for Controllable Gliding Flight
Wind Tunnel Test Report Conventional Model. Volume I. Low Speed Force and Moment Data
Wind Tunnel Test of a Model Utilizing Vectored Thrust for In-Flight Maneuverability
Wind-Tunnel Study to Explore the Use of Slot Spoilers to Modulate the Flap-Induced Lift of a Wing
Wind Tunnel Results of the High-Speed NLF(Natural Flow Control)(1)-0213 Airfoil