Controllability of the X-15 Research Airplane with Interim Engines During High-altitude Flights |
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Page 11
... artificial feel 10 ° single wedge 40.91 4.58 8.95 TABLE I.- PHYSICAL CHARACTERISTICS OF THE AIRPLANE Concluded - 10.21 11.
... artificial feel 10 ° single wedge 40.91 4.58 8.95 TABLE I.- PHYSICAL CHARACTERISTICS OF THE AIRPLANE Concluded - 10.21 11.
Page 12
... artificial feel Root chord , ft Tip chord , ft Taper ratio Aspect ratio • Sweep at 25 - percent - chord line , deg · Ratio vertical - tail area to wing area Movable surface area , sq ft Deflection , deg . Sweepback of hinge line , deg ...
... artificial feel Root chord , ft Tip chord , ft Taper ratio Aspect ratio • Sweep at 25 - percent - chord line , deg · Ratio vertical - tail area to wing area Movable surface area , sq ft Deflection , deg . Sweepback of hinge line , deg ...
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Common terms and phrases
25-percent-chord line Airfoil section airplane oscillation angle of attack angle of sideslip area Movable surface area to wing artificial feel boost with artificial center stick control deflection control task damping ratio deg Control system deg/deg/sec deg/sec due to full fixed-base flight simulator flight envelope flight gain flight plan flight-path angle ft Root chord ft Taper ratio ft Tip chord ft-lb g units high-altitude hinge line horizontal tail hypersonic inertia Irreversible hydraulic boost Level flight lightly damped low dynamic pressure Mach number maximum Mean aerodynamic chord minimum dynamic pressure moment of inertia Movable surface area NASA normal acceleration North American Aviation pilot was requested precise control pressure altitude pressure of 10.6 push-over ratio Aspect ratio reaction controls roll control slug-ft2 sq ft Deflection sq ft Span stabilizer deflection stabilizing the airplane Sweep at 25-percent-chord Taper ratio Aspect trajectory velocity wing area Movable X-15 airplane X-15 flight