guest
May 23rd, 2000, 10:52 AM
Seen that in a recent post (stieviboy May-21-00, 10:48 AM (PST) "opening speed") somebody (space) was asking for P.C.’s drag forces, I thought about posting this one.
The hereinafter reported formulas for freefall were reported on the BASE Board last year by a jumper (Basetroll ?), I implemented them on an Excel spreadsheet, plus I added the formula for air pressure and for resistance force caused by air pressure on a given surface, finally generating the hereinafter reported table which expresses the theoretical drag force exerted by a given ZP P.C. at a given airspeed. What I got are numbers that make sense. So here we go.
Please, forgive me for the form of present post, but I am not so clever in using the BASE Board editor for writing down formulas and tables.
ρair = 1.225 kg/m³ air density at sea level
cw = shape coefficient of skydiver body
mb = overall jumper body weight &l;kg&r;
A = jumper exposed surface &l;m²&r;
cw = 0.28 frog position
cw = 0.22 tracking position
cw = 0.18 head down position
g = 9.8 m/s² gravity acceleration
k = 0.5 · ρair · cw · A resistance coefficient &l;kg/m&r;
VL = sqrt(g · mb / k) terminal velocity &l;m/s&r;
Assumed a jumper of overall body weight mb = 80 kg in frog position (cw = 0,28 ) and of body surface A = 1.8 m², we shall have then:
k = 0.3087 kg/m
VL = 50.4 m/s
helping factor q = exp(VL · (2k/mb) · t)
a(t) = 4 · g· ( q / ((q 1)²) ) acceleration &l;m/s²&r;
v(t) = VL · ((q - 1)/(q 1)) velocity &l;m/s&r; or
v(t) = VL · tanh(VL · (k/m) · t) velocity &l;m/s&r;
s(t) = (VL²/(2 g)) · ln( ((q 1)²)/(4 q) ) distance &l;m&r;
P = ½ · ρair · v² air pressure &l;N/m²&r; (where v² is the square of velocity)
F(N) = P · APC where APC is the area of ZP P.C. in m²
F(kg) = F(N)/9.8
F(lb) = F(kg)/0.4536
m = 0.3048 · ft
ft = 3.2808 · m
m = 0.0254 · in
where m is meter, t is time expressed in seconds, s is second, kg is kilo, N is Newton, lb is pound, ft is feet, in is inch, ln is the natural logarithm, tanh is the hyperbolic tangent, sqrt is the square root, exp( x ) is what comes from e elevated to x (where e is the natural logarithm base (e = 2.718))
In the hereinafter reported table the drag force F is expressed in kg and is reported in the column headed by the diameter of ZP P.C. expressed in inches.
P. C.’s Drag Force Table
t s(t) v(t) a(t) P 48" 46" 45" 42" 40" 38" 36" 35" 32" 28"
&l;s&r; &l;m&r; &l;m/s&r; &l;m/s²&r; &l;N/m²&r; F F F F F F F F F F
0 0 0 9.8 0 0 0 0 0 0 0 0 0 0 0
0.5 1 5 9.7 15 1.7 1.6 1.5 1.3 1.2 1.1 1 0.9 0.8 0.6
1 5 10 9.4 57 6.8 6.3 6.0 5.2 4.7 4.3 3.8 3.6 3.0 2.3
1.5 11 14 9.0 125 15 14 13 11 10 9 8 8 7 5
2 19 19 8.5 213 25 23 22 19 18 16 14 14 11 9
2.5 29 23 7.8 317 38 35 33 29 26 24 21 20 17 13
3 42 26 7.1 429 51 47 45 39 35 32 29 27 23 17
3.5 56 30 6.4 545 65 60 57 50 45 41 37 35 29 22
4 72 33 5.6 660 79 72 69 60 55 49 44 42 35 27
4.5 89 35 4.9 771 92 84 80 70 64 58 52 49 41 31
5 107 38 4.3 874 104 96 92 80 72 65 59 55 46 35
6 147 41 3.2 1054 126 115 110 96 87 79 71 67 56 43
7 190 44 2.3 1196 142 131 125 109 99 89 80 76 63 48
8 235 46 1.6 1302 155 142 136 119 108 97 87 82 69 53
9 282 47 1.1 1379 164 151 144 126 114 103 92 87 73 56
10 330 48 0.8 1433 171 157 150 131 119 107 96 91 76 58
11 378 49 0.5 1472 175 161 154 134 122 110 99 93 78 60
12 428 49 0.4 1498 178 164 157 137 124 112 100 95 79 61
13 477 50 0.2 1516 181 166 159 138 125 113 102 96 80 61
14 527 50 0.2 1529 182 167 160 139 126 114 102 97 81 62
15 577 50 0.1 1537 183 168 161 140 127 115 103 97 81 62
16 627 50 0.1 1543 184 169 162 141 128 115 103 98 82 63
17 677 50 0.1 1547 184 169 162 141 128 116 104 98 82 63
18 728 50 0.04 1550 185 170 162 141 128 116 104 98 82 63
19 778 50 0.02 1552 185 170 162 142 128 116 104 98 82 63
20 828 50 0.02 1553 185 170 163 142 128 116 104 98 82 63
What I would like to point out about hereinabove reported table is that the drag force values are theoretical drag force values, in the sense that they are actuall drag force values if, and only if, you have an infinitely rigid disc (i.e., steel plate) put in an airstream (with its axis perfectly parallel to the airstream itself) at that given speed and having no burble in front of it.
So the most experienced BASE jumpers can (being perfectly right) argue that the reported drag force values must be diminished (of how much, I do not know !) taking into account that: 1) in front of the PC there is a small burble (jumper’s body), as smaller as longer the bridle is; 2) the fabric of PC is not ZP (Zero Porosity); 3) the actual diameter of inflated PC is different (=narrower) than the diameter of PC put at rest on the floor, depending on PC manufacture, etc.; 4) the axis of PC could be not parallel to air stream depending on jumper’s body position during freefall; 5) other factors.
So, please, equipment manufacturers or other experts can find and tell us the “diminishing factor” to be divided by above drag force values to generate the actual drag force values.
What above could be exact, not exact, close from being exact, far from being exact, I do not know.
But.
Stated all what above, one thing is for sure. The ratios between hereinabove reported drag force values are valid whichever the “diminishing factor” could be. Being the drag force proportional to P.C.’s surface, at any given air speed it is always true that a 48” has got 3 times the drag force than a 28”, and a 48” has got twice the drag force than a 35”.
(being the ‘at rest’ areas of above P.C.’s as follows: 48”: area = 1.17 m²; 35”: area = 0.62 m²; 28”: area = 0.40 m²).
All above said and done, I wish blue skies to you all
Andrea Checchia
The hereinafter reported formulas for freefall were reported on the BASE Board last year by a jumper (Basetroll ?), I implemented them on an Excel spreadsheet, plus I added the formula for air pressure and for resistance force caused by air pressure on a given surface, finally generating the hereinafter reported table which expresses the theoretical drag force exerted by a given ZP P.C. at a given airspeed. What I got are numbers that make sense. So here we go.
Please, forgive me for the form of present post, but I am not so clever in using the BASE Board editor for writing down formulas and tables.
ρair = 1.225 kg/m³ air density at sea level
cw = shape coefficient of skydiver body
mb = overall jumper body weight &l;kg&r;
A = jumper exposed surface &l;m²&r;
cw = 0.28 frog position
cw = 0.22 tracking position
cw = 0.18 head down position
g = 9.8 m/s² gravity acceleration
k = 0.5 · ρair · cw · A resistance coefficient &l;kg/m&r;
VL = sqrt(g · mb / k) terminal velocity &l;m/s&r;
Assumed a jumper of overall body weight mb = 80 kg in frog position (cw = 0,28 ) and of body surface A = 1.8 m², we shall have then:
k = 0.3087 kg/m
VL = 50.4 m/s
helping factor q = exp(VL · (2k/mb) · t)
a(t) = 4 · g· ( q / ((q 1)²) ) acceleration &l;m/s²&r;
v(t) = VL · ((q - 1)/(q 1)) velocity &l;m/s&r; or
v(t) = VL · tanh(VL · (k/m) · t) velocity &l;m/s&r;
s(t) = (VL²/(2 g)) · ln( ((q 1)²)/(4 q) ) distance &l;m&r;
P = ½ · ρair · v² air pressure &l;N/m²&r; (where v² is the square of velocity)
F(N) = P · APC where APC is the area of ZP P.C. in m²
F(kg) = F(N)/9.8
F(lb) = F(kg)/0.4536
m = 0.3048 · ft
ft = 3.2808 · m
m = 0.0254 · in
where m is meter, t is time expressed in seconds, s is second, kg is kilo, N is Newton, lb is pound, ft is feet, in is inch, ln is the natural logarithm, tanh is the hyperbolic tangent, sqrt is the square root, exp( x ) is what comes from e elevated to x (where e is the natural logarithm base (e = 2.718))
In the hereinafter reported table the drag force F is expressed in kg and is reported in the column headed by the diameter of ZP P.C. expressed in inches.
P. C.’s Drag Force Table
t s(t) v(t) a(t) P 48" 46" 45" 42" 40" 38" 36" 35" 32" 28"
&l;s&r; &l;m&r; &l;m/s&r; &l;m/s²&r; &l;N/m²&r; F F F F F F F F F F
0 0 0 9.8 0 0 0 0 0 0 0 0 0 0 0
0.5 1 5 9.7 15 1.7 1.6 1.5 1.3 1.2 1.1 1 0.9 0.8 0.6
1 5 10 9.4 57 6.8 6.3 6.0 5.2 4.7 4.3 3.8 3.6 3.0 2.3
1.5 11 14 9.0 125 15 14 13 11 10 9 8 8 7 5
2 19 19 8.5 213 25 23 22 19 18 16 14 14 11 9
2.5 29 23 7.8 317 38 35 33 29 26 24 21 20 17 13
3 42 26 7.1 429 51 47 45 39 35 32 29 27 23 17
3.5 56 30 6.4 545 65 60 57 50 45 41 37 35 29 22
4 72 33 5.6 660 79 72 69 60 55 49 44 42 35 27
4.5 89 35 4.9 771 92 84 80 70 64 58 52 49 41 31
5 107 38 4.3 874 104 96 92 80 72 65 59 55 46 35
6 147 41 3.2 1054 126 115 110 96 87 79 71 67 56 43
7 190 44 2.3 1196 142 131 125 109 99 89 80 76 63 48
8 235 46 1.6 1302 155 142 136 119 108 97 87 82 69 53
9 282 47 1.1 1379 164 151 144 126 114 103 92 87 73 56
10 330 48 0.8 1433 171 157 150 131 119 107 96 91 76 58
11 378 49 0.5 1472 175 161 154 134 122 110 99 93 78 60
12 428 49 0.4 1498 178 164 157 137 124 112 100 95 79 61
13 477 50 0.2 1516 181 166 159 138 125 113 102 96 80 61
14 527 50 0.2 1529 182 167 160 139 126 114 102 97 81 62
15 577 50 0.1 1537 183 168 161 140 127 115 103 97 81 62
16 627 50 0.1 1543 184 169 162 141 128 115 103 98 82 63
17 677 50 0.1 1547 184 169 162 141 128 116 104 98 82 63
18 728 50 0.04 1550 185 170 162 141 128 116 104 98 82 63
19 778 50 0.02 1552 185 170 162 142 128 116 104 98 82 63
20 828 50 0.02 1553 185 170 163 142 128 116 104 98 82 63
What I would like to point out about hereinabove reported table is that the drag force values are theoretical drag force values, in the sense that they are actuall drag force values if, and only if, you have an infinitely rigid disc (i.e., steel plate) put in an airstream (with its axis perfectly parallel to the airstream itself) at that given speed and having no burble in front of it.
So the most experienced BASE jumpers can (being perfectly right) argue that the reported drag force values must be diminished (of how much, I do not know !) taking into account that: 1) in front of the PC there is a small burble (jumper’s body), as smaller as longer the bridle is; 2) the fabric of PC is not ZP (Zero Porosity); 3) the actual diameter of inflated PC is different (=narrower) than the diameter of PC put at rest on the floor, depending on PC manufacture, etc.; 4) the axis of PC could be not parallel to air stream depending on jumper’s body position during freefall; 5) other factors.
So, please, equipment manufacturers or other experts can find and tell us the “diminishing factor” to be divided by above drag force values to generate the actual drag force values.
What above could be exact, not exact, close from being exact, far from being exact, I do not know.
But.
Stated all what above, one thing is for sure. The ratios between hereinabove reported drag force values are valid whichever the “diminishing factor” could be. Being the drag force proportional to P.C.’s surface, at any given air speed it is always true that a 48” has got 3 times the drag force than a 28”, and a 48” has got twice the drag force than a 35”.
(being the ‘at rest’ areas of above P.C.’s as follows: 48”: area = 1.17 m²; 35”: area = 0.62 m²; 28”: area = 0.40 m²).
All above said and done, I wish blue skies to you all
Andrea Checchia