Constraint.default: Default Classified list for constraint analysis

In HaoLi111/rAviExp: Aviation Exploratory

Default Classified list for constraint analysis

Description

Restrictions of a project. The parameters mainly restrict kinetic properties.

Usage

data("Constraint.default")

Format

The format is:
List of 8
$ W_S : num [1:451] 5 5.1 5.2 5.3 5.4 5.5 5.6 5.7 5.8 5.9 ...(List of W_S, wing loading to calculate)
$ TURN :List of 6 (Conditions for a ;evel, constant speed turn)
..$ Cd_min: num 0.02(minimum Drag coefficient)
..$ v : num 20(translational speed of the turn)
..$ H : num 200(Height,not required if q is calculated)
..$ k : num 0.0398(lift induced drag factor)
..$ n : num 0.357(load factor)
..$ q : num 240(kinetic density)
$ ENERGY_LEVEL :List of 8 (Conditions for a specific energy Level)
..$ Cd_min: num 0.02(minimum Drag coefficient)
..$ k : num 0.0398(lift induced drag factor)
..$ n : num 0.181(load factor)
..$ Ps : num 1(Energy level, the extra power that is availiable at this state)
..$ v : num 20(speed)
..$ H : num 200(Height)
..$ rho : num 1.2(Density, can be calculated from H, is used to calculate q)
..$ q : num 240
$ CLIMB :List of 7
..$ v_v : num 5(Rate of climb, vertical component of velocity)
..$ v : num 15(total velocity)
..$ k : num 0.0398
..$ Cd_min: num 0.02
..$ H : num 200
..$ q : num 135
..$ rho : num 1.2
$ CRUISE_V :List of 7
..$ H : num 200
..$ k : num 0.0398
..$ Cd_min: num 0.02
..$ v : num 20(Cruise Speed)
..$ H : num 200
..$ rho : num 1.2
..$ q : num 240
$ SERVICE_CEILING:List of 6
..$ v_v : num 20
..$ Cd_min: num 0.02
..$ H : num 400
..$ k : num 0.0398
..$ rho : num 1.18
..$ q : num 236
$ CL_MAX_STALL :List of 1
..$ q: num 50(kinetic density at the desired speed and height)
$ TO_DISTANCE :List of 8
..$ ClTO: num 1.2(Take-off Cl, usually when flap-on)
..$ CdTO: num 0.5(Take-off Cd, usually when flap-on)
..$ H : num 0
..$ v : num 20
..$ SG : num 30(Ground running distance)
..$ mew : num 0.2(Friction coefficient)
..$ rho : num 1.22
..$ q : num 245
- attr(*, "class")= chr "Constraint"

Details

The format is:
List of 8
$ W_S : num [1:451] 5 5.1 5.2 5.3 5.4 5.5 5.6 5.7 5.8 5.9 ...(List of W_S, wing loading to calculate)
$ TURN :List of 6 (Conditions for a ;evel, constant speed turn)
..$ Cd_min: num 0.02(minimum Drag coefficient)
..$ v : num 20(translational speed of the turn)
..$ H : num 200(Height,not required if q is calculated)
..$ k : num 0.0398(lift induced drag factor)
..$ n : num 0.357(load factor)
..$ q : num 240(kinetic density)
$ ENERGY_LEVEL :List of 8 (Conditions for a specific energy Level)
..$ Cd_min: num 0.02(minimum Drag coefficient)
..$ k : num 0.0398(lift induced drag factor)
..$ n : num 0.181(load factor)
..$ Ps : num 1(Energy level, the extra power that is availiable at this state)
..$ v : num 20(speed)
..$ H : num 200(Height)
..$ rho : num 1.2(Density, can be calculated from H, is used to calculate q)
..$ q : num 240
$ CLIMB :List of 7
..$ v_v : num 5(Rate of climb, vertical component of velocity)
..$ v : num 15(total velocity)
..$ k : num 0.0398
..$ Cd_min: num 0.02
..$ H : num 200
..$ q : num 135
..$ rho : num 1.2
$ CRUISE_V :List of 7
..$ H : num 200
..$ k : num 0.0398
..$ Cd_min: num 0.02
..$ v : num 20(Cruise Speed)
..$ H : num 200
..$ rho : num 1.2
..$ q : num 240
$ SERVICE_CEILING:List of 6
..$ v_v : num 20
..$ Cd_min: num 0.02
..$ H : num 400
..$ k : num 0.0398
..$ rho : num 1.18
..$ q : num 236
$ CL_MAX_STALL :List of 1
..$ q: num 50(kinetic density at the desired speed and height)
$ TO_DISTANCE :List of 8
..$ ClTO: num 1.2(Take-off Cl, usually when flap-on)
..$ CdTO: num 0.5(Take-off Cd, usually when flap-on)
..$ H : num 0
..$ v : num 20
..$ SG : num 30(Ground running distance)
..$ mew : num 0.2(Friction coefficient)
..$ rho : num 1.22
..$ q : num 245
- attr(*, "class")= chr "Constraint"

Examples

create(Constraint.default)
## maybe str(Constraint.default) ; plot(Constraint.default) ...

HaoLi111/rAviExp documentation built on Oct. 21, 2022, 2:18 a.m.