Basic Model Airplane Proportions 1.01 review (mobile)
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.
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Basic Model Airplane Proportions 1.01 is cars/aircraft software developed by Kenneth Gilbert.
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.
This hobby software is shareware, which means you can download and use Basic Model Airplane Proportions 1.01 for free during the trial period (usually for 30 days). At the expiration of the period you will have to buy the cars/aircraft product for $12.00. Basic Model Airplane Proportions 1.01 is available at regnow and Kenneth Gilbert website.
Basic Model Airplane Proportions 1.01 supports english interface languages and works with PalmOS.
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Basic Model Airplane Proportions related software
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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.
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Wing Calculator 1.0
Calculates wing balance point, mean aerodynamic chord (MAC) & its location from root chord, wing sweep (+ or -) distance from MAC leading edge, wing area, and aspect ratio.
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Converts English or Metric data entered for a Model Airplane or Aircraft.
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Model Airplane Weight & Balance 1.01
Calculates Center of Gravity (CG) based on model weight + component weights and component distance from Datum (ARM).
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Model Airplane Scale Calculator 1.11
Scales data from the database to feet or inches and calculates wing and power loadings.


