1-17 of 17 Books
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
Collision with terrain
Collision with terrain
By Transportation Safety Board of Canada
Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing
Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing
By Daniel G. Murri

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
By Robert D. Van Dyken
Stall spin, Tail Winds Light Aircraft Inc., Aces High Cuby II (Advanced Ultralight) C-FQYD, Kenaston, Saskatchewan 8nm W, 15 May 1994
Stall spin, Tail Winds Light Aircraft Inc., Aces High Cuby II (Advanced Ultralight) C-FQYD, Kenaston, Saskatchewan 8nm W, 15 May 1994
By Transportation Safety Board of Canada
Predicting stall of a two-dimensional airfoil using an algebraic Reynolds stress model
Predicting stall of a two-dimensional airfoil using an algebraic Reynolds stress model
By Lars Davidson
Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane
Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane
By H. Paul Stough
Air Rainbow Ltd., Beechcraft (3T) Twin Beech 18 C-FRVR, Nanaimo, British Columbia, 27 January 1992
Air Rainbow Ltd., Beechcraft (3T) Twin Beech 18 C-FRVR, Nanaimo, British Columbia, 27 January 1992
By Transportation Safety Board of Canada
Suppression of dynamic stall by steady and pulsed upper-surface blowing
Suppression of dynamic stall by steady and pulsed upper-surface blowing
By D. Weaver
PIV-Messungen instationarer Geschwindigkeitsfelder an einem schwingenden Rotorprofil
PIV-Messungen instationarer Geschwindigkeitsfelder an einem schwingenden Rotorprofil
By Markus Raffel
Identification of aircraft stability derivatives for the high angle-of-attack regime
Identification of aircraft stability derivatives for the high angle-of-attack regime
By W. E. Hall
Stall at low altitude, Edmonton Flying Club, Bellanca 8KCAB Decathlon C-GWZE, Villeneuve, Alberta, 15 March 1994
Stall at low altitude, Edmonton Flying Club, Bellanca 8KCAB Decathlon C-GWZE, Villeneuve, Alberta, 15 March 1994
By Transportation Safety Board of Canada
Power loss/stall, Man-Air Services Ltd., Cessna 185C Skywagon C-GKLR, Cornish Lake, Ontario 2 nm NE, 19 May 1993
Power loss/stall, Man-Air Services Ltd., Cessna 185C Skywagon C-GKLR, Cornish Lake, Ontario 2 nm NE, 19 May 1993
By Transportation Safety Board of Canada
Stall during initial climb
Stall during initial climb
By Transportation Safety Board of Canada
Effect of an extendable slat on the stall behavior of a VR-12 airfoil
Effect of an extendable slat on the stall behavior of a VR-12 airfoil
By P. Plantin De Hugues
Stall/near stall investigation of the F-4E aircraft
Stall/near stall investigation of the F-4E aircraft
By Collet E. McElroy
Loss of control, Aerogolfe Ltee, De Havilland DHC-2 MK 1 Beaver C-FIUS, Petit Pas Lake, Quebec, 28 July 1993
Loss of control, Aerogolfe Ltee, De Havilland DHC-2 MK 1 Beaver C-FIUS, Petit Pas Lake, Quebec, 28 July 1993
By Transportation Safety Board of Canada