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مراجع

1 2  Crane, Dale: Dictionary of Aeronautical Terms, third edition, page 144. Aviation Supplies & Academics, 1997. (ردمك 1-56027-287-2)
↑  Location referred to half-span : Beech C23 0.54, Piper PA-28 0.55, Yankee AA-1 0.57, Cirrus SR20 0.61, Lancair 300 0.66, Questair Venture 0.70, Cessna 172 0.71 - according to SAE TP 2000-01-1691, page 14
↑  Cox، Jack (نوفمبر 1988). "Questair Venture, Part Two". مؤرشف من الأصل في 2021-08-02. اطلع عليه بتاريخ 2009-08-08.
↑  Stough, DiCarlo Spin Resistance Development for Small Airplanes - A Retrospective, SAE TP 2000-01-1691 or "Nasa Stall Spin Paper from 1970s, or .
↑  Nasa TP 2011 (Yankee AA-1), Nasa TP 2772 (Cessna 210)
↑  H. Paul Stough III and Daniel J. DiCarlo, Spin Resistance Development for Small Airplanes - A Retrospective, SAE TP series 2000-01-1691
↑  Kroeger, R. A.; and Feistel, T, Reduction of stall-spin Entry Tendencies Through Wing Aerodynamic Design, SAE paper 760481
↑  NASA TP 1589, Wind-Tunnel Investigation of a Full-Scale General Aviation Airplane Equipped With an Advanced Natural Laminar Flow Wing
↑  NASA TP 1589 : "The mechanism by which the outer-panel lift is maintained to such improved stall/spin characteristics has been unclear".
↑  NACA TN 423, Weick, Fred E. Investigation of lateral control near the stall flight investigation with a light high-wing monoplane tested with various amounts of washout and various lengths of leading-edge slot.
↑  Hoerner, Fluid Dynamic lift, 12-24
↑  Zimmerman, NACA TN 539, 1935, "Aerodynamic characteristics of several airfoils of low aspect ratio". "The preservation of unturbuled flow to very high angles of attack ... is apparently due to the action of the tip vortices in removing the boundary layer that ends to built up near the trailing edge of the upper surface of the airfoil".
↑  Addition of a fairing ... to eliminate the discontinuity reintroduced abrupt tip stall (SAE TP 2000-01-1691)
↑  Summary of results for spin attempts for four NASA research aircraft.,
↑  Barnaby Wainfan, KitPlanes July 1998, Wind Tunnel, Foiling stalls is the month's topic : "It has been found that the single-droop cuff configuration described in NASA TP 1589 is not sufficient to prevent spins on high ratio wings."
↑  Murri, Jordan, Nasa TP 2772, Wind-Tunnel Investigation of a Full-Scale General Aviation Airplane Equipped With an Advanced Natural Laminar Flow Wing (Cessna 210), Leading-Edge Modifications, p.9, "The data for the outboard-droop configuration show significantly enhanced roll damping characteristics at the stall; however, unstable roll damping characteristics are not completely eliminated with the outboard droop alone."
↑  NASA TP 2722, "... an unsteady stalling and reattaching behavior occurring inboard on the wing upper surface as wing stall progressed."
↑  Investigations of modifications to improve the spin resistance of a high-wing, single engine, light airplane, SAE Paper 891039 (1989)
↑  H. Holmes, Nasa's general aviation stall/spin program, Sport Aviation, January 1989
↑  Effects of Wing-Leading-Edge Modifications on a Full-Scale, Low-Wing General Aviation Airplane, Nasa TP 2011, Drag characteristics, p. 13
↑  Nasa TP 2691, Flight Investigation of the Effects of an Outboard
Wing-Leading-Edge Modification on Stall/Spin Characteristics of a Low-Wing, Single-Engine, T-Tail Light Airplane : "within the measurement accuracy, no difference was found in airplane drag for lift coefficients typical of cruising flight."
↑  "Spin Resistance" (PDF). whycirrus.com. مؤرشف من الأصل (PDF) في 2022-04-12.
↑  Rutan VariEze, NASA TP 2382 (1985) et NASA TP 2623 (1986)
↑  NASA TP 1589, Nasa TP 2011
↑  NASA CT 3636, NASA TP 2691
↑  SAE paper 891039
↑  AIAA 86-2596
↑  Sport Aviation Nov. 88. Meyer et Yip, AIAA 89-2237-CP report.
↑  NASA TP 2772
↑  DOT/FAA/CT-92/17, AIAA/FAA Joint symposium on GA
↑  "Data". grumman.net. مؤرشف من الأصل في 2021-07-24.
↑  Cessna (2009). "This beauty is more than skin deep". مؤرشف من الأصل في 2009-07-26. اطلع عليه بتاريخ 2009-08-08.
↑  Horton Inc (n.d.). "Description of the Horton STOL Kit". مؤرشف من الأصل في 2008-11-21. اطلع عليه بتاريخ 2009-08-08.