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how does high angle of attack make plane stall?

i still dont understand this? What does the high angle of attack have to do with the engine? my instructor keeps says it loses lift but i dont understand why it makes it stall?
does engine failure practice also make plane stall?

Your wing does not produces enough lift because there is too much resistance in the airflow of the airfoil of the aircraft that means that the relative wind is like hitting a big wall unlike if you have a lower angle of attack the relative wind flows smoothly

Angle Of Attack $15.65 Rated: NASynopsis: Angle of Attack chronicles the 100-year history of Naval aviation from wobbly gliders and the first shipboard landing in 1911 to modern supersonic jets and unmanned aerial vehicles. The two-hour program, deftly interweaves archival footage, interviews with historical and military experts, contemporary footage of cutting-edge aircraft and insights from today's Top Gun fighter pilots in the Marine Corps and Navy. From the battlefields of yesterday, today, and tomorrow, Angle of Attack provides stunning, previously unseen footage of the most modern naval military aircraft and advanced unmanned predator drones ever designed, as well as a sweeping journey through naval aviation history. Featuring interviews with aviation experts and the men who flew and designed the most important military aircraft of all time, Angle of Attack examines the role of naval aviation in each of our nation s greatest conflicts.

Angle of Attack $13.99 Track Listing: 1. Salvation, 2. X-Echo 1, 3. Create What You Fear, 4. Folks, Let's Nebulate, 5. Big Seth, 6. Sideways Savannah - (featuring Greg Gilmore), 7. Find the Key, 8. X-Echo 2, 9. Naive Bid for HM Stardom #2, 10. Angle of Attack, 11. Time is Running Out - (featuring Greg Gilmore), 12. Post-X - (featuring Greg Gilmore), 13. Naive Bid #1, 14. Bold Leaps of Unreason...(Part II) - (featuring Greg Gilmore)

Angle of Attack (DVD) $44.57 This 2011 documentary takes a two-pronged look at military history. It begins by profiling cutting edge footage of early 21st Century unmanned predator drones and naval military aircraft; it then reflects on decades of navial aviation to examine how various navy aircraft have evolved and developed over time, guided by tactical considerations and many other factors. This segment features extended interviews with pilots and military strategists, and also examines the pivotal roles that naval planes have played in several key global conflicts.

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Pressure Differential Angle of Attack Measuring System $116.3 The purpose of this research activity is towards identifying the location to install Flush Port Air Data System (FADS) on different aerodynamic shapes. FADS systems typically have in excess of 10 pressure ports/sensors. Flush Port Pressure Sensors are symmetrically placed on the airframe. The pressure measured at each port varies as the airframe manoeuvres. Pressure Difference between corresponding ports on top and bottom of an aerodynamic body correspond to changes in AoA. Potential Flow Theory can be used for preliminary analysis because of its linearity for predicting the flow behaviour on various simpler aerodynamic shapes e.g. cylinder, sphere, wedge, cone and airfoil. The flow patterns obtained from this theory are simulated in MatLab to calculate Pressure Differential variation with respect to AoA on them. Also the variations on these surfaces are then compared with one another to check whether the front part of these surfaces correspond to the same Pressure Differential or not. On the basis of this Pressure Differential Variation w.r.t AoA, the location to install the Pressure Differntial AOA measuring instrument is suggested. Author: Mughal, Umair Binding Type: Paperback Number of Pages: 128 Publication Date: 2010/06/20 Language: English Dimensions: 5.98 x 9.01 x 0.30 inches

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How does the angle of attack affect drag on an airfoil?

If you have specific data, please identify it.....

the greater angle of atack the more lift and drag you get. you cant calculate really calculate drag, people use wind tunnels for that but you can calulate the drag force. not sure what your using it for but mainly AOA is used in automotive and aeronomics. my old fluids book had a 1/2 page for this and used an airplane wing to show what i just said.

hope this helps ....

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