Arrow Weight and F.O.C Calculator

For XX78 Arrow

Arrow Weight: Grn

arrow.gif (3178 bytes)

Point
Weight
Point
Insert
Shaft
Type
Shaft
Length
Fletch
Type
Number of
Fletches
Nock
Adaptor
Nock
Size

After all selections have been made click here to calculate estimated FOC(Front of Center)

  % (See explanation below)

(C) 1999 All Rights Reserved by Steve Jackson.

 

Arrow Weight Calculator

For XX75 Arrows

Select component from menus below and Arrow Weight
will add up everytime a menu selection is changed.
If you do not have one of the components then leave the
default, it will not add any weight to the total. The fletch weights
are based on Trueflight Feathers(F) and Easton Vanes(V) these
were the only published weights that I could find.

Arrow Weight: Grn

arrow.gif (3178 bytes)

Point
Weight
Point
Insert
Shaft
Type
Shaft
Length
Fletch
Type
Number of
Fletches
Nock
Adaptor
Nock
Size

After all selections have been made click here to calculate estimated FOC(Front of Center)

  % (See explanation below)

(C) 1999 All Rights Reserved by Steve Jackson.

 

Arrow Weight Calculator

For Carbon Express Arrows

When selecting shafts and adaptors etc below;

CX = CX 3D Select and CX Black
LJ = Linejammer
CXH = CX Hunter 
TB = Terminator Black
TH = Terminator Hunter

Select component from menus below and Arrow Weight
will add up everytime a menu selection is changed.
If you do not have one of the components then leave the
default, it will not add any weight to the total. The fletch weights
are based on Trueflight Feathers(F) and Easton Vanes(V) these
were the only published weights that I could find.

Arrow Weight: Grn

arrow.gif (3178 bytes)

Point
Weight
Point
Insert
Shaft
Type
Shaft
Length
Fletch
Type
Number of
Fletches
Nock
Adaptor
Nock
Size

After all selections have been made click here to calculate estimated FOC(Front of Center)

  % (see explanation below)

(C) 1999 All Rights Reserved by Steve Jackson.

CALCULATION OF THE POSITION OF THE CENTRE OF PRESSURE

 

The following example of how to calculate an arrow center of pressure makes two basic simplifications. Firstly the arrow is assumed not to be rotating (fishtailing). If the arrow is rotating then the air velocity (and hence the drag) varies along the arrow. Secondly the shape of the fletchings is assumed to be a right angled triangle, the nearest simple shape that approximates to a fletching.

 

 cpocp3.gif (2960 bytes)

 

The approach is first to calculate the total pressure and center of pressure locations for the shaft drag, fletching drag and Munk moment individually and then calculate the arrow total pressure and center of pressure location from the three components.

In the diagram the total drag force (T) acts at the arrow center of pressure at distance (Lt) behind the center of gravity (C). The total drag is the sum of the fletching drag (Ff), the shaft drag (Fs) and the Munk moment (Fm). The distances from the center of gravity to the fletching drag, shaft drag and Munk moment centers of pressure are Lf, Ls and Lm respectively. The resulting axis of rotation of the arrow (R) is at a distance 'A' in front of the arrow center of gravity.

If you equate the moments for the arrow total pressure/center of pressure to the individual shaft/fletchings/Munk moment total pressures/centers of pressure you end up with the distance Lt being given by:-

Lt = (Fs Ls + Ff Lf - Fm Lm)/(Fs+Ff-Fm)

Example

 

Suppose the arrow is 80 cm long and 0.5 cm diameter. The arrow FOC is 13%. The fletchings are assumed to be 2.5 cm long with each fletching having a total area of 3.5 square cm. The front of the fletchings are fitted 73 cm from the front of the shaft. There are 3 fletchings fitted at 120 degrees to the shaft and they are assumed to be triangular in shape.

To make life simple it is assumed that the drag properties of the shaft and fletchings are identical so instead of drag forces we can use drag areas. (main difference is in the shaft and fletching drag coefficients).

With an FOC of 13% the center of gravity is 10.4 cm in front of the center of the shaft.

Munk Moment

 

The value of Fm is assumed at 1.5 square cms. (based on some rough measurements made some years ago).The center of pressure is assumed to act at the back of the arrow so Lm = 80/2 + 10.4 = 54 cms.

Shaft Drag

 

The shaft area contributing to rotational drag Fs = 2 x 10.4 x 0.5 = 10.4 square cms. (see section on FOC). Because of symmetry the distance Ls is half the shaft length i.e. 40 cms

fletching

For a triangular fletching the centre of pressure horizontal position is 2/3 distance along the base from the front. (The vertical position doesn't matter as the fletchings are assumed not to be spinning the arrow)

i.e. Lf = 73 + 2.5 x 2 / 3 - (40-10.4) = 45.07 cms

The effective area Ff of the fletchings = 1.5 x 3.5 = 5.25 square cms.

(the multiplier 1.5 allows for the fletching angle = 2 x sin squared (alpha/2) where alpha is the angle between fletching).

Lt is therefore (10.4 x 40 + 5.25 x 45.07 - 1.5 x 54)/(10.4 + 5.25 - 1.5) = 40.4 cms

i.e. the center of pressure is 40.4 centimeters behind the arrow center of gravity.

Any arrow rotation will have the effect of moving the center of pressure further back so the 40.4 cms represents the minimum distance between the center of gravity and the center of pressure. (With e.g. fishtailing the influence of the shaft drag decreases and the influence of the fletching drag and Munk moment increases)

If 'Ig' is the arrow moment of inertia at the center of gravity and 'M' is the total arrow mass then the distance of the arrow axis of rotation in front of the center of gravity 'A' is given by:-

A = Ig / (Lt x M)

e.g. if Ig was 5400 gm cm squ. and M was 18 gms then A = 5400/(40.4 x 18) = 7.4 cms

 

 

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