CTOL Transport Technology, 1978: Proceedings of a Conference Held at Langley Research Center, Hampton, Virginia, February 28-March 3, 1978, Part 2

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National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978 - Aerodynamics - 982 pages

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active controls technology aerodynamic aeroelastic aileron air transportation airfoil airline airplane altitude analysis angle ANOPP approach aspect ratio baseline basic bending moment benefits Boeing characteristics chord concepts configuration crosswind landing crosswind landing-gear cruise CTOL drag Effect of Winglets engine evaluation Figure 11 flap flight tests flutter flying qualities frequency gust load high-aspect-ratio supercritical wing high-lift system improvement inboard increase indicated interference drag jet transports JET-A KEAS landing gear Langley Research Center lift coefficient load alleviation system Mach number maneuver load mode nacelle NASA noise prediction outboard ailerons percent performance pitch potential propfan reduced reference requirements runway safety semispan shown in figure simulation SMALL TAIL span speed spoilers structural weight supercritical wing take-off terminal area tip extensions touchdown turbulence U.S. Customary Units vortex minimization wind shear wind tunnel wing load alleviation wing-tip extensions winglets

Bibliographic information

TitleCTOL Transport Technology, 1978: Proceedings of a Conference Held at Langley Research Center, Hampton, Virginia, February 28-March 3, 1978, Part 2
CTOL Transport Technology, 1978: Proceedings of a Conference Held at Langley Research Center, Hampton, Virginia, February 28-March 3, 1978, United States. National Aeronautics and Space Administration
Volume 2036 of NASA conference publication
ContributorUnited States. National Aeronautics and Space Administration
PublisherNational Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
Original fromthe University of California
DigitizedApr 14, 2008
Length982 pages
  
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