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Aviation History
1926
1926 - 1015.PDF
107 DECEMBER 30, 1926 CHIBITED AT mver /h.p. •40 •36 •80 •60 •37 •34 ;-38 ,•49 •66 •05 •32 •44 •72 •44 •68 -5 •74 •87 •54 •0 •64 •20 •<; •27 •33 •88 •21 •33 •98 •43 •55 •62 •26 •81 •75 •75 •98 •02 •23 •44 •26 •m •72 114 31 i7 • 15 "»6 ••58 i U Loading. lbs./h.p. (141) ( 9-6) (10-6) (7-92) (14-0) (13-97) (7-45) (14-3) (21-3) (8-9) (18-3) (11-9) (14-8) (14-2) (10-3) (12-2) (21-4) (30-5) (10-0) (15-4) (14-6) (9-25) (14-3) (11-6) (18-3) (21-7) (7-05) (11-7) (8-75) (14-1) (14-4) (16-8) (7-17) (12-8) (17-0) (19-2) (8-37) (8-28) (7-10) (9-74) (11-6) (19.1) (10-4) (15-5) (13-9) (12-4) (15-9) (10-0) (10-3) (11-0) (20-3) ("•56) THE Wing Loading. kg./sq.m 420 47-3 60-0 73-5 46-3 61-5 41-2 45-7 42-6 54-3 78-8 49-0 51-4 50-0 44-6 38-5 29-2 27-7 48-7 35-0 63-2 65-6 61-5 43-2 28-7 22-6 64-2 40 0 49-7 45-0 51-6 49 • 9 54-8 53 1 47-2 38-9 61-2 57-0 66-5 42-8 50-6 75-7 67-4 .58-7 53-1 40-0 73-0 51-3 52-7 47-9 32-6 65 0 .lbs./sq.ft. (8-60) (9-68) (12-55) (15-0) (9-43) (12-6) (8-42 (9-38) (8-77) (11-1) (161) (10-0) (10-5) (10-2) (9-12) (7-86) (5-98) (5-67) (9-95) (7-16) (12-9) (13-4) (12-6) (8-82) (5-85) (4-63) (13-1) (8-17) (10-1) (9-2) (11-4) (10-9) (11-2) (10-8) (9-65) (7-94) (11-9) (12-1) (13-6) (8-73) (10-4) (15-2) (13-7) (12-0) (10-8) (8-16) (14-9) (10-4) (10-7) (9-77) (6-64) (13-3) THE AIRCRAFT PARIS AIR SHOW Span - •' Wing hp./.-sq.m. i 0-52 0-42 0 • 59 0-35 0 • 62 0 • 36 0-44 0-47 0 • 75 0-34 — 0-44 — 0-35 0-53 0-52 0-67 1-16 0-21 0-50 0-38 0-41 0-51 0 • 67 0-51 0-65 0-42 0-43 0-37 0-38 0-46 0-39 0-53 0 • 54 0 • 60 0 • 78 0-58 0 • 37 0-38 0-48 0-41 0-27 0-53 0-40 0-41 0-52 0-38 0-40 0-34 0-52 0-88 0-41 6-56 10-85 12-50 20-40 7-26 9-68 12-2 7-0(5 4-41 13-4 9-47 9-00 7-64 7-76 9-55 6-92 3-00 200 10-7 5-00 9-52 15-6 9-49 9-18 3-44 2-29 20'0 7-50 12-5 7-00 7-92 6-54 16-8 9-13 6-09 4-44 15-4 15-7 20 • 6 9 • 63 9 • 63 8-73 14-3 8-33 8-41 7-06 10-5 11-2 11-2 9-58 3-53 18-9 Power." li.p./sq.ft. (0-61) (1-01) (1-19) (1-90) (0-67) (0-90) (1-13) (0-66) (0-41) (1-24) (0-88) (0-84) (0-71) (0-72) (0-89) (0-64) (0-28) (0-19) (0-99) (0-46) (0-88) (1-45) (0-88) (0-76) (0-32) (0-21) (1-86) (0-70) (1-16) (0-64) (0-73) (0-61) (1-56) (0-85) (0-57) (0-41) (1-43) (1-46) (1-91) (0-87) (0-87) (0-80) (1-33) (0-77) (0-78) (0-66) (0-98) (1-04) (1-04) (0-89) (0-33) (1-76) Max. km. h. 215 225 240 270 163 180 283 180 100 240 200 204 170 209 180 142 125 230 186 202 255 185 207 120 120 260 185 215 180 192 170 250 245 267 275 217 215 200 220 190 186 200 235 218 224 225 140 222 , 1926 Speed, 1 Level. m.p.h. (130) (U0) (149) (167-6) (101) (112) (176) (112) (99-5) (149) (124) (127) (115) (130) (112) (88-2) (77-7) (143) (116) (125) (158) (115) (128) (74-5) (74-5) (161) (115) (134) (112) (119) (106) (155) (152) (166) (171) (135) (134) (124) (137) (118) (115) (124) (146) (135) (139) (140) (87-0) (138) ENGINEER Climb Alti. (m.) 5.000 in 5,000 in 5 000 in 5.000 in 2,000 in — — — 2.000 in 5,000 in — 4.000 in — 3.000 in 5.000 in — — — 5,000 in 4.000 in 3.000 in 5,000 in 3.000 in — — — 5,000 in 3,000 in — — — — 5,000 in — — — — 5.000 in 6.500 in 5,000 in — — 5,000 in — 4,000 in 4.000 in — 6,000 in 6,500 in — 1.000 in 5,000 in mins. 19-3 24 16 12-5 12 12 20 30 35 28-8 24-9 30 27-4 17 22-2 14 20 12 13-05 40-23 20-35 20-2 56 28-5 29 43 6 15-3 SUPPLEMENT TO FLIGHT Ceiling. High-speed m. 7.600 (5.000 7 500 7.500 4.200 12,442 4.000 7,000 5,600 4.000 6.375 3.200 2,600 (i.000 4.300 6.700 4.700 6.500 4.000 5.500 7.500 9.750 8,600 8,000 7,400 5,800 2,500 7,150 4,400 5,500 4,800 6,250 6,500 3,500 8,500 ft. (24,900) (19.700) (24.600) (24.600) (13.800) (40,800) (13,120) (23,000) (18,350) (13.120) (20.900) (10.500) (8,525) (19.700) (14.100) (22.000) (15.400) (21.300) (13J2O) (18.000) (24,(500) (32,000) (28,200) (26,200) (24,300) (19.000) ( ,200) (23,500) (14,430) (18,000) (15,750) (20,500) (21,300) (11,500) (27.900) Figure. 27-0 19-2 20-0 19-5 10-8 11 -0 34-5 150 170 18-5 — 16-0 19-5 11-5 16-5 15-2 17-5 18-5 20-5 23-0 15-5 190 12-3 170 9-5 13-8 15-6 15-0 14-3 15-2 16-3 17-0 16-5 — — — 17-0 22 0 18-0 190 18-5 16-5 13-3 15 0 14-0 21-0 22 0 16-0 18-0 20-8 14-0 10-5 Altitude Figure. 9-4 5-1 S • 5 7-0 5-2 — * — 7 '5 61 — 6-0 — 5-4 5 • 6 — 5 • 3 li-li — 7-0 6-5 6-7 6-9 6-5 — 5-4 — 5-2 6-3 — — — 8-5 — — 8-6 6-8 — 6-4 6- * 8-2 — 5-8 5-5 8-1 5-8 — 6-5 5-5 7 • 7 * Falls outside graph.
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