Basic Model Airplane Proportions 1.01

Basic Model Airplane Proportions (BMAP) is designed to calculate the data input for Engine CID, Model Weight, Wing Area, Wing Loading, Power Loading, Wing Root Chord, Wing Tip Chord, and Wing Span into measurements needed for model fabrication. All the above can be calculated based on related data entered or you can enter your own. Default values for the above are also available for various engine sizes. Calculations: Mean Aerodynamic Chord (MAC) Aspect Ratio (AR) Taper Ratio (TR) 15% Forward Center of Gravity (FWD CG) 25% Center of Gravity (CG) 30% AFT Center of Gravity (AFT CG) 35% Neutral Point (NP) Distance from CG for Propeller, 25% MAC, and 25% Horizontal Stabilizer MAC MAC distance from Root Chord Wing Dihedral Wing Position: High, Middle, Low Standard and Strip Aileron Measurements

Horizontal Stabilizer and Elevator Area Vertical Stabilizer and Rudder Area (with or without ailerons) Other associated programs available are Aircraft Scale Calculator (ASC) and Model Airplane Weight & Balance (MAWB) These programs are a must have for the model airplane builder.