blob: 99335935f18b660ac9bcdef39c6aa09e26a067e8 (plain)

ofs	hex dump	ascii
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0540	5f 63 6c 61 73 73 5f 5f 72 13 00 00 00 72 14 00 00 00 72 15 00 00 00 46 00 00 00 73 0e 00 00 00	_class__r....r....r....F...s....
0560	00 03 12 02 08 02 06 01 06 02 06 02 06 02 7a 10 41 69 72 66 6f 69 6c 2e 5f 5f 69 6e 69 74 5f 5f	..............z.Airfoil.__init__
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0760	54 68 69 73 20 66 75 6e 63 74 69 6f 6e 20 67 65 6e 65 72 61 74 65 73 20 67 65 6f 6d 65 74 72 79	This.function.generates.geometry
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07c0	70 65 72 66 6f 72 6d 20 74 68 65 20 72 65 71 75 69 72 65 64 20 73 74 65 70 73 20 74 6f 20 67 65	perform.the.required.steps.to.ge
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0860	65 20 72 65 74 72 69 65 76 65 64 20 66 72 6f 6d 20 57 69 6b 69 70 65 64 69 61 2e 6f 72 67 2e 0a	e.retrieved.from.Wikipedia.org..
0880	0a 20 20 20 20 20 20 20 20 50 61 72 61 6d 65 74 65 72 73 3a 0a 20 20 20 20 20 20 20 20 6e 61 63	.........Parameters:.........nac
08a0	61 5f 6e 75 6d 3a 20 34 2d 64 69 67 69 74 20 4e 41 43 41 20 77 69 6e 67 0a 20 20 20 20 20 20 20	a_num:.4-digit.NACA.wing........
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0900	4e 6f 6e 65 0a 20 20 20 20 20 20 20 20 72 01 00 00 00 e9 64 00 00 00 e9 01 00 00 00 e9 0a 00 00	None.........r.....d............
0920	00 e9 02 00 00 00 4e 63 01 00 00 00 00 00 00 00 03 00 00 00 05 00 00 00 13 00 00 00 73 be 00 00	......Nc....................s...
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09c0	00 18 00 64 02 88 01 14 00 7c 00 88 03 6a 01 1b 00 14 00 17 00 7c 00 88 03 6a 01 1b 00 64 02 13	...d.....|...j.......|...j...d..
09e0	00 18 00 14 00 7d 02 6e 08 74 02 64 04 83 01 01 00 7c 01 7c 02 88 03 6a 01 14 00 66 02 53 00 29	.....}.n.t.d.....|.|...j...f.S.)
0a00	05 7a 5b 0a 20 20 20 20 20 20 20 20 20 20 20 20 52 65 74 75 72 6e 73 20 31 20 63 61 6d 62 65 72	.z[.............Returns.1.camber
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0a40	68 65 20 61 69 72 66 6f 69 6c 20 63 68 6f 72 64 2e 0a 20 20 20 20 20 20 20 20 20 20 20 20 72 01	he.airfoil.chord..............r.
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0ae0	03 70 5f 63 72 12 00 00 00 72 13 00 00 00 72 14 00 00 00 da 0a 67 65 74 5f 63 61 6d 62 65 72 70	.p_cr....r....r......get_camberp
0b00	00 00 00 73 16 00 00 00 00 04 04 01 06 01 18 01 1a 01 14 01 1a 01 02 01 0c 01 30 02 08 02 7a 20	...s......................0...z.
0b20	41 69 72 66 6f 69 6c 2e 6e 61 63 61 2e 3c 6c 6f 63 61 6c 73 3e 2e 67 65 74 5f 63 61 6d 62 65 72	Airfoil.naca.<locals>.get_camber
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0b60	64 01 7c 00 04 00 03 00 6b 01 72 1c 88 00 6a 01 6b 01 72 86 6e 04 01 00 6e 66 64 02 88 01 14 00	d.|.....k.r...j.k.r.n...nfd.....
0b80	88 00 6a 01 14 00 64 03 74 02 7c 00 88 00 6a 01 1b 00 83 01 14 00 64 04 7c 00 88 00 6a 01 1b 00	..j...d.t.|...j.......d.|...j...
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0bc0	64 08 13 00 14 00 17 00 64 09 7c 00 88 00 6a 01 1b 00 64 0a 13 00 14 00 18 00 14 00 7d 01 6e 08	d.......d.|...j...d.........}.n.
0be0	74 03 64 0b 83 01 01 00 7c 01 53 00 29 0c 7a 4f 0a 20 20 20 20 20 20 20 20 20 20 20 20 52 65 74	t.d.....|.S.).zO.............Ret
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0c20	74 68 65 20 61 69 72 66 6f 69 6c 20 63 68 6f 72 64 2e 0a 20 20 20 20 20 20 20 20 20 20 20 20 72	the.airfoil.chord..............r
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0c80	e9 04 00 00 00 7a 47 78 2d 63 6f 6f 72 64 69 6e 61 74 65 20 66 6f 72 20 74 68 69 63 6b 6e 65 73	.....zGx-coordinate.for.thicknes
0ca0	73 20 69 73 20 6f 75 74 20 6f 66 20 62 6f 75 6e 64 73 2e 20 43 68 65 63 6b 20 74 68 61 74 20 30	s.is.out.of.bounds..Check.that.0
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0d00	14 00 00 00 da 0d 67 65 74 5f 74 68 69 63 6b 6e 65 73 73 82 00 00 00 73 0e 00 00 00 00 04 06 01	......get_thickness....s........
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0dc0	22 64 02 88 00 14 00 64 03 88 01 18 00 64 02 13 00 1b 00 88 01 7c 00 88 03 6a 01 1b 00 18 00 14	"d.....d.....d.......|...j......
0de0	00 7d 01 7c 01 53 00 29 04 7a 4d 0a 20 20 20 20 20 20 20 20 20 20 20 20 52 65 74 75 72 6e 73 20	.}.|.S.).zM.............Returns.
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0e60	04 72 2c 00 00 00 72 2d 00 00 00 72 2e 00 00 00 72 12 00 00 00 72 13 00 00 00 72 14 00 00 00 da	.r,...r-...r....r....r....r.....
0e80	08 67 65 74 5f 64 79 5f 63 93 00 00 00 73 0c 00 00 00 00 04 06 01 18 01 20 01 1a 01 22 01 7a 1e	.get_dy_c....s..............".z.
0ea0	41 69 72 66 6f 69 6c 2e 6e 61 63 61 2e 3c 6c 6f 63 61 6c 73 3e 2e 67 65 74 5f 64 79 5f 63 63 01	Airfoil.naca.<locals>.get_dy_cc.
0ec0	00 00 00 00 00 00 00 02 00 00 00 02 00 00 00 53 00 00 00 73 0c 00 00 00 74 00 7c 00 83 01 7d 01	...............S...s....t.|...}.
0ee0	7c 01 53 00 29 01 4e 29 01 72 05 00 00 00 29 02 72 22 00 00 00 72 23 00 00 00 72 13 00 00 00 72	|.S.).N).r....).r"...r#...r....r
0f00	13 00 00 00 72 14 00 00 00 da 09 67 65 74 5f 74 68 65 74 61 9e 00 00 00 73 04 00 00 00 00 01 08	....r......get_theta....s.......
0f20	01 7a 1f 41 69 72 66 6f 69 6c 2e 6e 61 63 61 2e 3c 6c 6f 63 61 6c 73 3e 2e 67 65 74 5f 74 68 65	.z.Airfoil.naca.<locals>.get_the
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0fa0	6a 05 7c 00 19 00 88 00 6a 02 7c 00 19 00 74 06 88 00 6a 04 7c 00 19 00 83 01 14 00 17 00 7d 02	j.|.....j.|...t...j.|.........}.
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0fe0	83 01 14 00 18 00 7d 01 64 01 7d 02 7c 01 7c 02 66 02 53 00 29 02 4e 72 01 00 00 00 29 07 72 29	......}.d.}.|.|.f.S.).Nr....).r)
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1040	00 00 00 da 15 67 65 74 5f 75 70 70 65 72 5f 63 6f 6f 72 64 69 6e 61 74 65 73 a2 00 00 00 73 12	.....get_upper_coordinates....s.
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1080	61 63 61 2e 3c 6c 6f 63 61 6c 73 3e 2e 67 65 74 5f 75 70 70 65 72 5f 63 6f 6f 72 64 69 6e 61 74	aca.<locals>.get_upper_coordinat
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