(32SII) Glide Slope Calculations

08142023, 02:42 AM
Post: #1




(32SII) Glide Slope Calculations
Introduction
The following program calculates the forces and angle for a flight of a glider, an aircraft without a engine: * Weight * Lift Force * Drag Force SI units are used. With inputs glide distance (G), height (H), and mass (M): Angle: A = arcsin(H ÷ G) Weight: W = M × 9.80665 Lift: L = W × sin A Drag: D = W × cos A The program uses the polartorectangular conversion to calculate lift and drag. HP 32SII Programs: Glide Slope Calculations Code 1: Code: G01 LBL G Bytes: 42.5 Checksum: 4717 Notes: * This version has prompts and view commands to guide the user. We don't have to preload registers as the INPUT commands guide us. * All inputs and outputs are stored to variables. 7 variables are used, which will require 56 bytes. On the HP 32SII, each variable that contains nonzero values takes 8 bytes of memory. If you want to make the variables local, insert a CLVARS command for G23 and line G24 becomes RTN. Variables: Input: G = Glide Distance. The distance that glider climbs to it's peak. Think of the hypotenuse of a right triangle. Distance is in meters. H = Height. The height that the glider reaches. Distance is in meters. M = Mass. Mass of the glider in kilograms. Output: A = Angle. Angle of the of glider's flight in degrees. W = Weight. Weight of the glider, which is Newtons. L = Lift force of the glider, in Newtons. D = Drag force of the glider, in Newtons. Code 2: Code 2 is a shorter code which does not store anything into variables. The program starts with G (glide distance), H (height), and M (mass) on the stack. Code: L01 LBL L Bytes: 27.5 bytes Checksum: 6446 Examples Example 1: Glider distance: G = 178 m Height: H = 23 m Mass of the glider: M = 55 kg Output: Angle: A ≈ 7.4241° Weight: W ≈ 539.3658 N Lift: L ≈ 534.8441 N Drag: D ≈ 69.6933 N Example 2: Glider distance: G = 200 m Height: H = 30 m Mass of the glider: M = 39 kg Output: Angle: A ≈ 8.6269° Weight: W ≈ 382.4594 N Lift: L ≈ 378.1322 N Drag: D ≈ 57.3689 N Source National Museum of the United States Air Force. "Mathematics of Flight: Glide Slope II" September 2020. Retrieved August 2023. https://www.nationalmuseum.af.mil/Portal...e%20II.pdf What do you prefer: (1) programs with prompts and stores the results or (2) programs that uses the stack and saves as much memory as possible? 

06162024, 04:19 AM
Post: #2




RE: (32SII) Glide Slope Calculations
Wonder if this would work for a 747 with total engine failure.


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