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Blaicher B-38

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0.7 m/s (140 ft/min) minimum at 70 km/h (43 mph; 38 kn), flaps up. With flaps down, 0.4 m/s (79 ft/min) at 40 km/h (25 mph; 22 kn).
133:, flown by Zbigniew Źabski. After some modifications it was ready for official testing in August 1939 but was destroyed in the German invasion the following month. 121:, Michal Blaicher turned to a new design incorporating Fowler flaps. Construction began in the ZASPL workshops but moved when ZASPL became LWL, controlled by 130: 449: 392: 122: 444: 272: 125:, delaying its completion. Its first flight was made either late in 1938 or in the spring of 1939 at 205: 197: 384: 377: 118: 8: 211:
A detachable, two-wheeled trolley was used for take-off and a sprung skid for landings.
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J, Cynk (1971), except where noted. Performance from samolotypolskie
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instrumentation, was enclosed and had a long dorsal
97:
completed in 1938. Notable for its use of long span
204:surfaces were ply-covered and the control surfaces 376: 173:structure of oval cross-section. Its single seat 313:best 29 at 80 km/h (50 mph; 43 kn) 307:200 km/h (120 mph, 110 kn) in dive 436: 169:The glider's fuselage was a ply-covered, semi- 117:Following the WOS-37, his development of the 27:High performance, single seat, experimental 112: 218: 437: 370: 368: 366: 364: 362: 360: 358: 356: 325:35 km/h (22 mph; 19 kn) 192:was mounted above the fuselage on the 166:filled the remaining 2/3 of the span. 412: 410: 408: 406: 404: 383:. London: Putnam Publishing. p.  374: 353: 101:, its development was ended by the 13: 401: 262:1.25 m (4 ft 1 in) 256:16.3 m (53 ft 6 in) 147:and covered with stress-relieving 14: 461: 268:13.4 m (144 sq ft) 250:6.3 m (20 ft 8 in) 214: 1: 346: 450:Aircraft first flown in 1938 7: 329: 185:behind it. At the rear the 10: 466: 379:Polish Aircraft 1893-1939 289:275 kg (606 lb) 283:190 kg (419 lb) 200:were tab assisted. Fixed 18: 196:; like the ailerons the 136:The all-wood B-38 had a 69:Late 1938 or early 1939 445:1930s Polish sailplanes 235:General characteristics 224: 162:and, inboard of them, 113:Design and development 222: 375:Cynk, Jerzy (1971). 311:Maximum glide ratio: 109:in September 1939. 119:Czerwiński CW 5 bis 303:Never exceed speed 225: 177:, which included 158:were assisted by 143:built around two 83: 82: 457: 429: 428: 426: 424: 414: 399: 398: 382: 372: 297: 237: 76: 61:Michal Blaicher 40: 32:Type of aircraft 16: 15: 465: 464: 460: 459: 458: 456: 455: 454: 435: 434: 433: 432: 422: 420: 416: 415: 402: 395: 373: 354: 349: 341:List of gliders 332: 293: 233: 217: 115: 74: 39:National origin 38: 33: 12: 11: 5: 463: 453: 452: 447: 431: 430: 400: 393: 351: 350: 348: 345: 344: 343: 331: 328: 327: 326: 323:Minimum speed: 320: 314: 308: 291: 290: 284: 278: 269: 263: 257: 251: 245: 223:B-38 in flight 216: 215:Specifications 213: 206:fabric-covered 114: 111: 93:, single seat 81: 80: 77: 71: 70: 67: 63: 62: 59: 55: 54: 51: 47: 46: 41: 35: 34: 31: 25: 21: 20: 19:Blaicher B-38 9: 6: 4: 3: 2: 462: 451: 448: 446: 443: 442: 440: 419: 413: 411: 409: 407: 405: 396: 394:0 370 00085 4 390: 386: 381: 380: 371: 369: 367: 365: 363: 361: 359: 357: 352: 342: 339: 338: 337: 336: 335:Related lists 324: 321: 318: 317:Rate of sink: 315: 312: 309: 306: 304: 300: 299: 298: 296: 288: 287:Gross weight: 285: 282: 281:Empty weight: 279: 276: 274: 270: 267: 264: 261: 258: 255: 252: 249: 246: 243: 240: 239: 238: 236: 231: 229: 221: 212: 209: 207: 203: 199: 195: 191: 188: 184: 180: 176: 172: 167: 165: 161: 157: 154: 153:mass balanced 150: 146: 142: 139: 134: 132: 128: 124: 120: 110: 108: 104: 100: 96: 92: 88: 87:Blaicher B-38 78: 73: 72: 68: 66:First flight 65: 64: 60: 57: 56: 52: 50:Manufacturer 49: 48: 45: 42: 37: 36: 30: 26: 23: 22: 17: 421:. Retrieved 378: 334: 333: 322: 316: 310: 301: 294: 292: 286: 280: 273:Aspect ratio 271: 265: 259: 253: 247: 241: 234: 232: 227: 226: 210: 179:blind flying 168: 164:Fowler flaps 160:Flettner tab 135: 116: 105:invasion of 99:Fowler flaps 86: 84: 75:Number built 418:"B-38,1939" 295:Performance 439:Categories 423:28 October 347:References 266:Wing area: 187:cantilever 138:cantilever 254:Wingspan: 228:Data from 202:empennage 198:elevators 190:tailplane 171:monocoque 141:gull wing 95:sailplane 58:Designer 29:sailplane 330:See also 156:ailerons 260:Height: 248:Length: 183:fairing 175:cockpit 149:plywood 131:Skiłnów 391:  151:. The 107:Poland 103:German 91:Polish 89:was a 53:ZASPL 44:Poland 385:703-4 242:Crew: 145:spars 24:Role 425:2018 389:ISBN 127:Lwów 85:The 244:One 194:fin 123:PWS 441:: 403:^ 387:. 355:^ 277:20 208:. 79:1 427:. 397:. 305:: 275:: 129:-

Index

sailplane
Poland
Polish
sailplane
Fowler flaps
German
Poland
Czerwiński CW 5 bis
PWS
Lwów
Skiłnów
cantilever
gull wing
spars
plywood
mass balanced
ailerons
Flettner tab
Fowler flaps
monocoque
cockpit
blind flying
fairing
cantilever
tailplane
fin
elevators
empennage
fabric-covered

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