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Collision with terrain
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Stall during initial climb
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2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
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Effect of an extendable slat on the stall behavior of a VR-12 airfoil
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Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane
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Stall spin, Tail Winds Light Aircraft Inc., Aces High Cuby II (Advanced Ultralight) C-FQYD, Kenaston, Saskatchewan 8nm W, 15 May 1994
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Power loss/stall, Man-Air Services Ltd., Cessna 185C Skywagon C-GKLR, Cornish Lake, Ontario 2 nm NE, 19 May 1993
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Identification of aircraft stability derivatives for the high angle-of-attack regime
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Suppression of dynamic stall by steady and pulsed upper-surface blowing
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Stall/near stall investigation of the F-4E aircraft
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Stall at low altitude, Edmonton Flying Club, Bellanca 8KCAB Decathlon C-GWZE, Villeneuve, Alberta, 15 March 1994
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Experimental and computational analysis of separation bubble behavior for compressible, steady and oscillatory flows over a NACA 0012 airfoil at M=0.3 and a reynolds number of 540,000
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PIV-Messungen instationarer Geschwindigkeitsfelder an einem schwingenden Rotorprofil
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Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing
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Air Rainbow Ltd., Beechcraft (3T) Twin Beech 18 C-FRVR, Nanaimo, British Columbia, 27 January 1992
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Loss of control, Aerogolfe Ltee, De Havilland DHC-2 MK 1 Beaver C-FIUS, Petit Pas Lake, Quebec, 28 July 1993
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Predicting stall of a two-dimensional airfoil using an algebraic Reynolds stress model
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