Ogive Nose Cones
The ogive nose cone is probably one of the most common shapes used in model rocketry. It exhibits very good drag characteristics for general model rocketry use. If you are building a scale Tomahawk, Sandhawk, or Phoenix, then you will be dealing with an ogive. Ogives are classified by their "caliber”, or length to diameter ratio. Thus a nose that is one inch diameter and three inches long is a “3to1” (3:1) ogive and has a caliber of 3.
Once, while trying to build a NikeTomahawk, I tried to find the formula to draw a 3:1 ogive so that I could turn the cone on a lathe. I looked though Pete Alway’s The Art of Scale Model Rocketry, engineering and math textbooks, the CRC math handbook, old rocketry magazines, and the Internet. I could not find the formulas.
I decided to derive the equations myself. Step 1: What the heck is an ogive anyway? Webster’s Ninth Collegiate Dictionary defines “ogive” as “\‘oh,jiv\ n 1. a: a diagonal arch or rib across a Gothic vault b: a pointed arch 2: a graph each of whose ordinates represents the sum of all the frequencies up to and including a corresponding frequency in a frequency distribution”.
That didn't help much! Searching math and statistics sites turned up an explanation of the term "ogive" which can be found here at MathWorld, or here. They weren't much help in figuring out what an ogive nose cone is.
Further searching turned up an old NAR Technical Report #8: "Ogive’ me a ringtailed cylindrical bird says G. Harry Stine", and a description of ogive nose cones is given as follows:
"There are two basic types of ogival nose shapes: the tangent ogive and the secant ogive. A tangent ogive has an arc which meets the body contour smoothly, thereby creating no break in line where the ogive joins the cylindrical body. In other words, the center of rotation of the arc is in the plane of the base of the nose. If the center of rotation of the arc is aft of the plane of the base of the nose, you’ve got a secant ogive. Simple, no?"
This has been the only definition of a secant ogive I could find. The following diagrams illustrate what G. Harry was saying:
Figure 1. 
Figure 2. 
Using Figure 1 and Figure 3, along with some mathematical maneuvering, you can derive equation (1a). As my math professors in college were so fond of saying, "the solution to that exercise will be left to the student to complete…" (or see Appendix A). So now we know what an ogive curve is. (as related to rocket nose cones)
The following methods describe ways to calculate the centers and radii of the tangent, and secant ogive curves.
Tangent Ogive (numerical method)
The formula to generate a tangent ogive cone is:
_{} (1a)
where x, y are coordinates, x being along the length of the cone, and y being the "height" (or radius) of the cone taken from the centerline of the cone.
The caliber of the cone is:
_{} (2)
Where:
L = cone length
d = cone base dia
A simpler approximation formula can also be used:
_{} (1b) (This parabolic equation produces a slightly “flatter” curve than the arc equation.)
Note these equations will form 1/2 of the cone, you will need to mirror the plot to make the complete cone.
Equations 1a or 1b will provide x,y coordinates to machine a cone either manually, or by a numerical controlled (NC) lathe.
Tangent Ogive (graphical method, layout Figure 3)
This method was originally described in the Estes Technical Report TR11: Aerodynamic Drag of Model Rockets, by Dr. Gerald Gregorek. In that report, the offset K and radius R were given as constants for 3:1 and 2:1 ogive contours. To obtain similar relations for any caliber of ogive curve, see Appendix A:
Figure 3. 
Vertical offset = _{} (3)
Radius = _{} (4)
Caliber = _{} (5)

Secant Ogive (Derived from existing design, such as a scale rocket blueprint)
This is more involved to create than a tangent ogive. You have to find the center of rotation of the arc and determine how far aft it is from the plane of the base of the nose (xoff and yoff in the figure below). Then you will basically have a tangent ogive at an imaginary diameter, d2 (see layout, Figure 4).
1. Draw a line from the point of the nose to the intersection of the body tube (see close up Figure 5, below). This is called a chord, or a secant (imagine that!).
2. Find the center of the chordal length ( c ) and draw a perpendicular line (90 degrees) that crosses the curve of the nose cone.
3. Measure the perpendicular distance ( h ), and calculate the radius of the curve using the following formula:
_{} (6)
4. Now calculate the angle between the secant and the centerline of the nose ( b ), and the angle between the perpendicular and the radial line running from the nose tip to the center of the arc ( a/2 ):
_{} (7)
_{} (8)
Figure 4. 
Figure 5. 
5. Now calculate xoff and yoff to determine where the center of the arc is in relation to the base of the nose, and the centerline of the body:
_{} (9)
_{} (10)
6. At this point, you can draw the secant ogive cone using a compass. If you want to determine the true tangent ogive diameter, use the following:
_{} (11)
7. Now if you want to calculate x and y coordinates for a CAD program or NC lathe, use the tangent ogive equations from above, starting at x = xoff and use d2 for d.
Virginia Tech has a website on aerodynamics called "Configuration Aerodynamics Course" that has a pdf file called "Geometry for Aerodynamicists". This document contains formulas for other nose shapes, such as the Von Karmen ogive. It is 79 KB, and is available at http://www.dept.aoe.vt.edu/~mason/Mason_f/ConfigAeroAppA.pdf .
Another source of equations for other nose cone shape can be found at the VCP website. or from Wikipedia
David Stribling
NAR 18402 Sr.
http://rocketguy101.jimdo.com/
References
1. Ogive’ me a ringtailed cylindrical bird says G. Harry Stine; Stine, G.H.; NAR Technical Report #8
2. Aerodynamic Drag of Model Rockets; Gregorek, Gerald; Estes Industries TR11, 1970.
Derivation of the Ogive Equation
The equation of a circle is _{}
or, _{}
@ x=0, _{}, _{} or _{}
@ x=L, Ybar = K, _{}
Since R = R_{0} = R_{L}
_{}
Square both sides and cancel terms:
_{}
_{} becomes _{}
_{}
Substitute caliber_{} or L = C x d
and K becomes:
_{}
Therefore _{}
Substitute K back into the equation for R_{0}
_{}
_{}
_{}
Referring back to the figure, y = Ybar – K
_{}
_{}
substitute K and R from above,
_{}