Structures: V-n Diagrams Lecture 18 ME EN 415 Andrew Ning - - PowerPoint PPT Presentation
Structures: V-n Diagrams Lecture 18 ME EN 415 Andrew Ning - - PowerPoint PPT Presentation
Structures: V-n Diagrams Lecture 18 ME EN 415 Andrew Ning aning@byu.edu Safety Factor B777 Wing Bending https://youtu.be/Ai2HmvAXcU0 25.303 Factor of safety. Unless otherwise specified, a factor of safety of 1.5 must be applied to the
Safety Factor
https://youtu.be/Ai2HmvAXcU0 B777 Wing Bending
§25.303 Factor of safety. Unless otherwise specified, a factor of safety of 1.5 must be applied to the prescribed limit load which are considered external loads on the structure.
Air Speed
True airspeed (TAS): speed of aircraft relative to air Equivalent airspeed (EAS): airspeed at sea level with equivalent dynamic pressure 1 2ρTAS2 = 1 2ρSLEAS2 EAS = TAS r ρ ρSL
Design airspeeds (all in EAS)
VA : VB : Vs : VC : VD :
V-n Diagram
V (EAS) n VD VC nmmax stall stall
V-n Diagram
V (EAS) n VD VC nmmax stall stall
V-n Diagram
V (EAS) n VD VC nmmax stall
except that n may not be less than 2.5 and need not be greater than 3.8
stall
V-n Diagram
V (EAS) n VD VC nmmax stall stall
V-n Diagram
V (EAS) n VD VC nmmax stall
From an initial condition of stabilized flight at VC/MC, the airplane is upset, flown for 20 seconds along a flight path 7.5° below the initial path, and then pulled up at a load factor of 1.5g (0.5g acceleration increment). The speed increase occurring in this maneuver may be calculated if reliable or conservative aerodynamic data is used.