The F/A-18 High-Angle-of-Attack Ground-to-Flight Correlation; Lessons LearnedNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997 - Aerodynamics - 44 pages |
Common terms and phrases
8ƒLE 8ƒTE accurate prediction aft end Alpha Research Vehicle angles of attack boom boundary-layer C₁ canopy coefficient Daniel G Daniel W David F Dryden Flight Research dynamic pressure Erickson F-18 High Alpha F/A-18 aircraft F/A-18 configuration fineness ratio Fisher flare Flight Research Center flight tests forebody flow field forebody vortices Gary E geometry Grit pattern Nosering ground-to-flight correlation Hampton high angles High-Alpha Research Vehicle High-Angle-of-Attack Technology Conference higher Reynolds number interaction Laminar separation Langley Research Center lateral stability lateral-directional aerodynamics lateral-directional stability leading-edge flap deflection lift coefficient Mach number maximum lift MD/Navy Murri NASA Dryden Flight NASA Langley Research nose noseboom Nosering only Twin off-surface flow visualization on-surface flow pitching pitching moment pressure ports shown in figure significant sub-scale suction peaks surface pressure distribution Tail Buffet tunnel and flight twin strips visualization of NASA visualization was obtained Vortex Flow Vortex footprint wind tunnel