[aerohead]

I'll start this today,although it's doubtful that I'll get any images up today.
Some of my references to developing the 'Template' are from Hucho,who in turn cites Sighard Hoerner's 'Aerodynamic Drag.'
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I pulled out 5-figures from Hoerner's book which impact the 'Template':
*Fig.3.23 The drag of a Fuselage body the trailing end of which is cut off in steps.

*Fig. 5.11 Drag coefficient of three-dimensional bodies,based upon their wetted area,depending upon the Reynolds number.

*Fig. 5.12 The drag coefficient of three-dimensional bodies ( at supercritical Reynolds number ),based upon their wetted area,depending upon the thickness ratio.

*Fig.5.13 Frontal drag coefficient of three-dimensional bodies,depending upon their fineness ratio.

*Fig. 5.15 Drag coeffiient of three-dimensional bodies at a subcritical Reynolds number of R= 10,000
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Research data for the tables was assembled from reports by:
* AVA Gottingen
* DVL (Germany's NASA)
* Jahrb.Schiffbautech
* Kosin & Lehmann,Jahrb. D. Lufo.
* Massachusetts Institute of Technology
* NACA ( NASA ) Variable-Density Wind Tunnel
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Some of the streamline body ( airship) research for Fig.5.13 was conducted by Abbott,co-author of 'Theory of Wing Sections.'
-------------------------------------------------------------------------- I'll get the scans done as Al's work schedule permits.Appreciate your patience.
PS the images are quite small.If anyone wants to volunteer to Photo-Bucket them at a larger image scale,send me a PM with your mailing address and I'll get them to you.Thanks!