'Stall speed' diaporamas de présentation

Final Review Commercial

Final Review Commercial. Power Plants. Carburetor Heat Mixture. Fuel Injection. Auxiliary Fuel Pump Fuel Flow Indicator Vapor Lock Exhaust Gas Temperature Cylinder Head Temperature. Mixture. Best Economy Mixture Best Power Mixture. Abnormal Combustion. Preignition Detonation.

1.34k views • 121 slides

A- Lift equals weight and thrust equals drag. B- Lift, drag, and weight equal thrust.

#3205. What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?. A- Lift equals weight and thrust equals drag. B- Lift, drag, and weight equal thrust. C- Lift and weight equal thrust and drag. Sorry that is Incorrect.

1.06k views • 102 slides

Steep Turns

Steep Turns. Knowledge of Elements. Turning performance limits Power of the engine load factor limits aerodynamic characteristics Overbanking Tendency. Knowledge of Elements. Static Stability shallow turn - plane tries to return to wings level medium turn - plane remains in medium bank.

902 views • 76 slides

Quiz 3

Quiz 3. Aerodynamics. 1. [14] Gleim #: 1.7.40 -- Source: FTH Chap 17 If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays A. neutral longitudinal static stability. B. neutral longitudinal dynamic stability.

823 views • 62 slides

Basic Aerodynamics

1.17k views • 39 slides

Chandelles

Chandelles. Objective. Exhibit knowledge of the elements related to the performance factors associated with chandelles Obtain the maximum performance of the airplane:. Objective. the airplane should gain the most altitude possible for the degree of bank and power setting without stalling

484 views • 33 slides

Torque Converters

Torque Converters. Purpose. Allow the vehicle to come to a complete stop without stalling the engine Provide torque multiplication to allow smooth acceleration from a stop House a torque converter clutch which will eliminate torque converter slippage at highway speeds.

1.57k views • 33 slides

Predicting Performance

Predicting Performance. Density Altitude. Pressure altitude corrected for nonstandard temperature. Density Altitude. High Hot Humid. Density Altitude. Common methods of calculating include: Flight computer Density Altitude Chart. Density Altitude.

471 views • 26 slides

Wingman -22

Wingman -22. Qi Chengzi Arnab Roy Trevor Steiner. Improved fuel weight method. As the PI includes the max range of the missions, an improved method with integrating the Weight decreasing of the fuel burn is introduced, so that the PI can be increased.

433 views • 23 slides

System Requirements Review

Team 5. System Requirements Review. Robert Aungst Chris Chown Matthew Gray Adrian Mazzarella. Brian Boyer Nick Gohn Charley Hancock Matt Schmitt. Contents. Problem Definition Product Overview Business Case Competition Customer Attributes Design Requirements. Problem Definition.

788 views • 23 slides

Stability and Flight Controls

Stability and Flight Controls. Three Axes of Flight. Longitudinal (green) Nose to tail Lateral (blue) Wing tip to Wing tip Vertical (red) Top to bottom. Arm. Moment. Force. Glenn Fisher Private Pilot Ground School. Controls.

348 views • 21 slides

18-1 Sarah page Edwin Kumar peter Schneider rick prasad

18-1 Sarah page Edwin Kumar peter Schneider rick prasad. 154A Aircraft Design. Changing the Specs. Other STOL Planes . Picture of Mountain Goat STOL. Mountain Goal STOL. Max Gross Weight: 2500 lbs Wing Span: 35.5 ft Wing Area: 188 sq ft. Katmai STOL Plane with Canard.

377 views • 21 slides

System Definition Review

System Definition Review. Miguel Alanis Aaron Mayne Tim Block Jason Olmstead Becca Dale Adeel Soyfoo Joseph Fallon Sarah Weise. Review of Market. Air charters, governments (surveying, mail), medical transport, or supplies delivery companies

310 views • 19 slides

406.08 Loads and Load Factors

406.08 Loads and Load Factors. 1 X 40 min OCdt Marl-e-a-u. Outline. Definitions Relationship Between Wing Loading and Angle of Bank Load Factor in Turns Centripetal and Centrifugal Force Forces on Aircraft. What is weight?.

1.2k views • 19 slides

Wingman-22: Airfoil selection

Wingman-22: Airfoil selection. Arnab Roy Chengzhi Qi. Wing Design Process. High Wing. Geometry. Increases the dihedral effect. It makes the aircraft laterally more stable . (fuselage will also make contribution) Eases and facilitates to maintenance.

524 views • 18 slides

Automatic Transmissions

655 views • 15 slides

Lesson 14: Weight And Balance

Lesson 14: Weight And Balance. Importance Of Weight And Balance. Forward CG Increases tail down force which increases effective weight (real weight + tail down force) All parameters of aircraft performance will decrease except maximum power off glide distance. Importance Of Weight And Balance.

785 views • 15 slides

Wing Loading

414 views • 11 slides

SIERRA Aircraft and Payload Status

SIERRA Aircraft and Payload Status. Wing Span Length Height Wing Area Empty Weight Gross Weight Max Speed Cruise Speed Stall Speed (clean) Aspect ratio Rate of Climb CG Position Payload weight Payload power Duration. 20 ft. 11.8 ft. 4.6 ft. 42.4 sq. ft. 215 lbs. 375 lbs.

222 views • 6 slides