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Subsections


14. Appendix


14.1 Making support tubes / sheaths

14.1.1 Introduction

When routing the control wires of for the elevator and rudder on the QFII, they need to be secured in such a way that when the wire is under compression it doesn't buckle out, causing a loss of control. For wire diameters of 0.6mm or less it can often be difficult to locate suitable tubing for reinforcement so the natural solution is to make our own.

14.1.2 Requirements

10cm length of wire of one size larger than you plan to use for your control wires (ie, 0.8mm for 0.6mm controls)

Very thin paper (cigarette wrapping papers are excellent for this)

Gum glue or PVA

Clean wood or cork block

14.1.3 Procedure

14.2 Common product names

14.3 Commonly used Terms and Acronyms

AUW
All Up Weight; commonly used to describe the total weight of a plane in flying condition, ie complete with radio gear, batteries and anything else required to fly
CF
Carbon Fiber; A very popular material used for its extremely high tensile strength. CF is not good however for shock or compression loads.
CG
Center of Gravity (CoG); commonly refers to the longitudinal (pitching) static mass balance point of the aircraft. Typically the CG is determined by balancing the plane on two points located along the wing surface. A plane is considered to be ``nose heavy'' if the aircraft pitches its nose downwards at a given balance point or ``tail heavy'' if the tail of the aircraft pitches down. There is also a latitudinal static balance point, typically indicating which wing is heavier.
FG
Fiberglass; made of thousands of strands of very fine glass fiberglass is an extremely versatile material which only recently has been supplanted in some areas by carbon fiber cloth.
L/D
Lift Drag ratio; The L/D is a term commonly used with gliders when talking about the ``optimal L/D'' ratio. There are two points of particular interest with L/D, at the optimal ratio, the distance travelled is maximised, referred to as Vbg (Velocity of Best Glide), there is also Vmd (Velocity of Minimum Decent), at this velocity your glider will remain in the air longer but it will not cover as much distance.
LE
Leading Edge; This refers to the front edge of the flying surface
TE
Trailing Edge; This refers to the rear edge of the flying surface
TLAR
``That looks about right''; A somewhat humored term referring to a design process whereby the designer has chosen a particular design mostly based on its appearances. The more experienced the designer the better their TLAR design ability typically.

14.4 Conversions

14.4.1 Lengths and sizes

Please note these values are approximations only.

Metric Length Imperial
0.8mm

14.4.2 Weights

Please note these values are approximations only.

Metric weight Imperial
28.35g

14.5 Further information

QFII Website http://www.pldaniels.com/flying/models/qfii


next up previous contents index
Next: Index Up: QuickFlick-II Build manual Previous: 13. Flying
Paul Daniels
2005-09-15