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Armstrong Whitworth A.W.52

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268:, being powered by either six or four engines, which were buried within the wing as to not disturb the airflow over the exterior surfaces. It had to be relatively large in comparison with any prior flying wing in order to provide sufficient headroom for passengers to be realistically carried. Thus, the proposed airliner had an weight of around 180,000 lb and a span of at least 160 ft. Furthermore, its structure was to possess relatively little weight due to the absence of a traditional fuselage or tail unit. However, this radical design would need to be tested exhaustively, which ought to include the test flying of scale aircraft. The initial design for such an aircraft was designated as the 508: 362: 39: 484: 226:, during the 1920s and early 1930s. However, in spite of this early start, various difficulties inherent to the configuration repeatedly resulted in such efforts being abandoned without anything beyond experimental flying occurring. during the mid-1940s, Armstrong Whitworth became interested in the value of combining the flying wing configuration with that of two recent innovations: the 346:, which operated differentially, with a greater angle on the outer one. Roll and pitch were controlled with elevons that extended inward from the wing tips over most (in the case of the A.W.52 about three-quarters) of the outer, swept part of the trailing edge. The elevons moved together as elevators and differentially as ailerons. They were quite complicated surfaces – which included 350:– and hinged not from the wing but from "correctors", which were wing-mounted; the correctors provided pitch trim. To delay tip stall, air was sucked out of a slot just in front of the elevons, by pumps powered by undercarriage-mounted fans on the glider and directly from the engine in the A.W.52. The inner centre section wing carried 257:, in which it was determined that positive performance gains were achieved, but that these were rapidly diminished as dirt accumulated on the wing and disturbed the airflow. Lloyd calculated that, the adoption of a relatively clean tailless layout in combination with a laminar wing would generate only one-third of the aerodynamic 158:, which indicated that, in combination with the flying wing configuration, such an aircraft could be dramatically more efficient than traditional designs. It was pursued to gather data and experience with the configuration in support of Armstrong Whitworth's ambitions to develop its proposed flying wing 405:
engines, each capable of providing up to 3,500 lbf (16 kN). Trials of the two prototypes were largely disappointing: laminar flow could not be maintained, thus maximum speeds, though respectable, were less than had been expected. It was concluded that laminar flow could not be maintained on
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by a British pilot. The first prototype recovered and descended to the ground relatively undamaged. Shortly thereafter, Armstrong Whitworth decided to terminate all development work, having lost confidence in the configuration's practicality and the envisioned flying wing airliner that the A.W.52 was
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with relatively little damage. Following this incident, and in view of the relatively disappointing results that had been gathered so far, Armstrong Whitworth's management decided that no further effort would be exerted on the development of the flying wing concept. The company opted to allocate its
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Maintenance of laminar flow over the wings was vital to the design and so they were built with great attention to surface flatness. Rather than the usual approach, where skinning is added to a structure defined by ribs, the A.W.52's wings were built in two halves (upper and lower) from the outside
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The A.W.52 was intended for high speed research and designed as an all-metal turbojet-powered aircraft, with a retractable undercarriage. Aerodynamically, it had much in common with the glider, both aircraft being moderately-swept flying wings with a centre section having a straight trailing edge.
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While the glider had provided valuable data on the configuration's low speed characteristics, it was not capable of the high speed flight necessary to garner all of the needed data. For this, the production of self-propelled aircraft would be necessary. During late 1944, the Ministry of Supply had
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was designed. This glider was roughly half the size of the powered A.W.52, which in turn would be about half the size of the airliner. It was recognised that a glider could be completed quicker than a powered aircraft, and provide valuable aerodynamic data to refine the design of the powered
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a flying wing as had been hoped. As in any tail-less aircraft, take-off and landing runs were longer than for a conventional aircraft (at similar wing loadings) because at high angles of attack, downward elevon forces were much greater than those of elevators with their large moment.
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follow-on aircraft, particularly in regards to control and stability. The A.W.52G was mainly made out of wood, and comprised three sections, a central unit with a nacelle for accommodating its two pilots, and the two outer wing sections. Control was achieved via two wing-tip
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bomber. Tug releases from 20,000 ft (6,100 m) gave the glider a flight time of around 30 min continued; flight testing proceeded with typically satisfactorily result up until 1947. It was subsequently put on static display outside the company's
389:, was close to the aircraft's central point, being slightly off-set to port. The engines were mounted in the wing centre section, close to the centre line and so not disturbing the upper wing surface. To prevent tip stalling, a 400:
engines, each capable of generating a maximum of 5,000 lbf (22 kN) of thrust. Almost one year later, it was followed by the second prototype on 1 September 1948; it was instead propelled by a pair of lower-powered
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taken sufficient interest in Armstrong Whitworth's proposals that it issued a contract to the company for the production of a pair of two A.W.52 prototypes for evaluation purposes; they were nominally intended to serve as
441:, and thus became the first British pilot to use the apparatus in a "live" emergency. It was fortunate that Lancaster was alone in the aircraft, as the second crew member was never provided with an ejection seat. 312:
installed at the wing tips to aid in its recovery should pilots encounter severe difficulty in the aircraft's handling. Almost exactly two years later, on 2 March 1945, the glider conducted its
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in, starting from pre-formed surfaces, adding stringers and ribs then joining the two halves together. The result was a surface smooth to better than 2/1000 of an inch (50 
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within a nacelle so that the pilot was just forward of the wing's leading edge, providing a better view than in the glider. This cockpit, which was
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During March 1943, construction of the AW.52G commenced. It was decided that it should be built with a pair of anti-spin
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In order to test the design's low-speed characteristics, a single a 53 ft 10 in (16.41 m) span wooden
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NPL.655-3-218 at root, tapering to NPL.655-3-118 at extremity of the centre section and to NPL.654-3-015 at the tips
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of a conventional aircraft, and quickly began outlining an envisioned airliner that incorporated these features.
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Williams, Roy (December 1981 – March 1982). "Armstrong Whitworth's Flying Wings... A Tale of No Tails".
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Pelletier, Alain J. "Towards the Ideal Aircraft: The Life and Times of the Flying Wing, Part Two".
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Subsequently, the aircraft stopped fluttering and glided down and landed in open country north of
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with a request to design a full-scale wing suitable for conducting laminar flow drag tests in a
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In the aftermath of Armstrong Whitworth's withdrawal, the second A.W.52 was handed over to the
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On 30 May 1949, while diving the first prototype at 320 mph (510 km/h), test pilot
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intended to lead to. Despite the termination, the second prototype remained flying with the
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The first prototype performed its first flight on 13 November 1947, powered by a pair of
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An early design for this proposed airliner had emerged by 1943. It harnessed
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and two jet-powered aircraft, were constructed for the research programme.
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X-Planes of Europe: Secret Research Aircraft from the Golden Age 1946-1974
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seemingly imminent, Lancaster opted to eject from the aircraft using its
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Armstrong Whitworth AW-52 3-view drawing from Les Ailes 18 January 1947
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4,000 lb (1,800 kg) / 300 cu ft (8.5 m)
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aircraft designed and produced by British aircraft manufacturer
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2, pilot and navigator-wireless operator / flight test observer
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The wing tips carried small (not full chord) end-plate fin and
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Lancaster, Jo (October 2006). "Setting the Record Straight".
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airliner that featured a more conventional configuration.
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facility before being broken up during the late 1950s.
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500 mph (800 km/h, 430 kn) at sea level
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Aircraft of comparable role, configuration, and era
354:and the upper surface of the outer section carried 393:system, powered by the engines, was incorporated. 210:aircraft can be traced back to years prior to the 154:The A.W.52 emerged from wartime research into the 43:The second jet-powered A.W.52 with Derwent engines 1027:, No. 65, September–October 1996, pp. 8–19. 777: 2696: 1169: 951: 856: 854: 222:, to produce experimental aircraft such as the 835: 833: 823: 821: 712: 710: 172:On 13 November 1947, the A.W.52 performed its 1944: 1155: 1076: 994:. Manchester, UK: Hikoki Publications, 2015. 802: 800: 798: 796: 794: 792: 770: 768: 766: 744: 742: 740: 738: 728: 726: 724: 722: 628:1,500 mi (2,400 km, 1,300 nmi) 913: 851: 809: 640:4,800 ft/min (24 m/s) at sea level 882: 842: 830: 818: 707: 409: 1951: 1937: 1162: 1148: 1038: 789: 763: 757: 735: 719: 1041:British Research and Development Aircraft 869: 607:, 5,000 lbf (22 kN) thrust each 990:Buttler, Tony and Jean-Louis Delezenne. 646:24.8 lb/sq ft (121 kg/m) 506: 360: 1060:Armstrong Whitworth Aircraft since 1913 934:"The Incomplete Guide to Airfoil Usage" 927: 925: 519:Armstrong-Whitworth Aircraft since 1913 14: 2697: 1057: 1004: 783: 365:Model of the A.W.52 on display at the 1932: 1143: 523:The Incomplete Guide to Airfoil Usage 503:Specifications (TS 363, Nene powered) 922: 572:1,314 sq ft (122.1 m) 2710:1940s British experimental aircraft 560:89 ft 11 in (27.4 m) 24: 2269:de Havilland Canada DHC-1 Chipmunk 1962:manufactured in Britain since the 976:(1982): 673–679. 19 December 1946. 554:37 ft 5 in (11.4 m) 25: 2731: 1096: 931: 566:14 ft 5 in (4.4 m) 2425:Rolls-Royce Thrust Measuring Rig 482: 37: 984: 891: 593:34,150 lb (15,490 kg) 180:that motivated its test pilot, 2553:Scottish Aviation Twin Pioneer 1083:. No. 17. pp. 1–12. 1005:Mettam, H.A. (26 March 1970), 634:36,000 ft (11,000 m) 587:19,660 lb (8,918 kg) 301:were also installed along the 196: 13: 1: 2380:Fairey Ultra-light Helicopter 695: 690:List of experimental aircraft 201: 2720:Aircraft first flown in 1947 2705:Armstrong Whitworth aircraft 1171:Armstrong Whitworth Aircraft 700: 497:Royal Aircraft Establishment 475: 466:Royal Aircraft Establishment 251:National Physical Laboratory 191:Royal Aircraft Establishment 149:Armstrong Whitworth Aircraft 103:Royal Aircraft Establishment 81:Armstrong Whitworth Aircraft 7: 2284:British Aerospace Jetstream 1043:. G.T. Foulis. p. 45. 899:"THE 'FLYING WING' CRASHES" 656: 318:Armstrong Whitworth Whitley 10: 2736: 2508:Armstrong Whitworth Argosy 2325:Armstrong Whitworth A.W.52 2204: / anti-submarine 1995:English Electric Lightning 455:Armstrong Whitworth Apollo 275: 141:Armstrong Whitworth A.W.52 2654: 2571: 2548:Scottish Aviation Pioneer 2498: 2490:Youngman-Baynes High Lift 2313: 2234: 2200: 2182:English Electric Canberra 2162: 2092: 2033: 1970: 1896: 1875: 1854: 1808: 1782: 1746: 1730: 1698: 1667: 1660: 1539: 1264: 1188: 1177: 919:Tapper 1988, pp. 296-298. 860:Tapper 1988, pp. 292-293. 827:Tapper 1988, pp. 290-291. 815:Tapper 1988, pp. 288-290. 716:Tapper 1988, pp. 287-288. 422:believed to be caused by 336: 224:Westland-Hill Pterodactyl 129: 121: 116: 108: 98: 86: 74: 66: 53: 48: 36: 31: 2054:de Havilland Sea Vampire 527:Flight: 19 December 1946 410:Accident and termination 2538:Hawker Siddeley Andover 2136:Hawker Siddeley Harrier 2049:de Havilland Sea Hornet 1058:Tapper, Oliver (1988). 1039:Sturtivant, R. (1990). 1007:"The Pterodactyl Story" 938:m-selig.ae.illinois.edu 533:General characteristics 2410:Hawker Siddeley P.1127 2279:Handley Page Jetstream 2226:Hawker Siddeley Nimrod 2064:de Havilland Sea Vixen 2059:de Havilland Sea Venom 512: 453:resources towards the 391:boundary layer control 373: 331:mail carrying aircraft 2586:AgustaWestland Merlin 2581:AgustaWestland Apache 2533:Handley Page Hastings 1130:century-of-flight.net 650:Max lift coefficient: 510: 436:Martin-Baker Pre-Mk.1 416:John Oliver Lancaster 364: 182:John Oliver Lancaster 2674:Slingsby Grasshopper 2264:Boulton Paul Balliol 2084:Supermarine Scimitar 2079:Supermarine Attacker 1985:de Havilland Vampire 1265:Post-First World War 1126:British Flying Wings 1011:Flight International 888:Tapper 1988, p. 293. 848:Tapper 1988, p. 294. 839:Tapper 1988, p. 292. 806:Tapper 1988, p. 288. 774:Tapper 1988, p. 287. 748:Tapper 1988, p. 295. 732:Tapper 1988, p. 296. 228:laminar flow airfoil 156:laminar flow airfoil 2485:Supermarine Seagull 2435:Saunders-Roe SR.A/1 2395:Handley Page HP.115 2345:Blackburn Firecrest 2187:Handley Page Victor 2141:Panavia Tornado IDS 2126:Eurofighter Typhoon 2116:Blackburn Buccaneer 2020:Panavia Tornado ADV 2000:Eurofighter Typhoon 1980:de Havilland Hornet 1112:"The Airborne Wing" 468:and transferred to 403:Rolls-Royce Derwent 381:). The crew sat in 297:; a pair of Fowler 49:General information 2646:Westland Whirlwind 2611:Westland Dragonfly 2528:Blackburn Beverley 2440:Saunders-Roe SR.53 2390:Handley Page HP.88 2355:Boulton Paul P.120 2350:Boulton Paul P.111 1990:de Havilland Venom 1062:. London: Putnam. 901:. Our Warwickshire 513: 432:structural failure 426:. 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850: 841: 829: 817: 808: 788: 776: 762: 750: 734: 718: 705: 704: 702: 699: 697: 694: 693: 692: 681: 680: 678:Northrop YB-49 675: 673:Northrop XP-79 670: 658: 655: 654: 653: 647: 641: 638:Rate of climb: 635: 629: 623: 620:Maximum speed: 609: 608: 594: 588: 582: 573: 567: 561: 555: 549: 543: 504: 501: 500: 499: 493: 492: 490:United Kingdom 477: 474: 424:elevon flutter 418:encountered a 411: 408: 338: 335: 316:, towed by an 277: 274: 266:jet propulsion 203: 200: 198: 195: 135: 134: 131: 127: 126: 123: 119: 118: 114: 113: 110: 106: 105: 100: 96: 95: 90: 88: 84: 83: 78: 72: 71: 70:United Kingdom 68: 64: 63: 55: 51: 50: 46: 45: 42: 34: 33: 9: 6: 4: 3: 2: 2732: 2721: 2718: 2716: 2713: 2711: 2708: 2706: 2703: 2702: 2700: 2685: 2682: 2680: 2677: 2675: 2672: 2670: 2667: 2665: 2662: 2661: 2659: 2657: 2653: 2647: 2644: 2642: 2639: 2637: 2636:Westland Wasp 2634: 2632: 2629: 2627: 2624: 2622: 2621:Westland Lynx 2619: 2617: 2614: 2612: 2609: 2607: 2604: 2602: 2599: 2597: 2594: 2592: 2589: 2587: 2584: 2582: 2579: 2578: 2576: 2574: 2570: 2564: 2561: 2559: 2558:Short Belfast 2556: 2554: 2551: 2549: 2546: 2544: 2541: 2539: 2536: 2534: 2531: 2529: 2526: 2524: 2523:Beagle Basset 2521: 2519: 2516: 2514: 2511: 2509: 2506: 2505: 2503: 2501: 2497: 2491: 2488: 2486: 2483: 2481: 2478: 2476: 2473: 2471: 2470:Slingsby T.53 2468: 2466: 2465:Short Sperrin 2463: 2461: 2458: 2456: 2453: 2451: 2448: 2446: 2443: 2441: 2438: 2436: 2433: 2431: 2428: 2426: 2423: 2421: 2420:Hunting H.126 2418: 2416: 2413: 2411: 2408: 2406: 2405:Hawker P.1072 2403: 2401: 2400:Hawker P.1052 2398: 2396: 2393: 2391: 2388: 2386: 2385:Folland Midge 2383: 2381: 2378: 2376: 2373: 2371: 2368: 2366: 2363: 2361: 2358: 2356: 2353: 2351: 2348: 2346: 2343: 2341: 2338: 2336: 2333: 2331: 2328: 2326: 2323: 2322: 2320: 2318: 2314:Prototype and 2312: 2306: 2303: 2301: 2298: 2295: 2292: 2290: 2287: 2285: 2282: 2280: 2277: 2275: 2272: 2270: 2267: 2265: 2262: 2260: 2257: 2255: 2252: 2250: 2247: 2245: 2242: 2241: 2239: 2237: 2233: 2227: 2224: 2222: 2221:Fairey Gannet 2219: 2217: 2214: 2212: 2209: 2208: 2206: 2203: 2199: 2193: 2190: 2188: 2185: 2183: 2180: 2178: 2175: 2173: 2170: 2169: 2167: 2165: 2161: 2155: 2149: 2147: 2144: 2142: 2139: 2137: 2134: 2132: 2131:Hawker Hunter 2129: 2127: 2124: 2122: 2119: 2117: 2114: 2112: 2109: 2107: 2104: 2103: 2101: 2099: 2098:ground attack 2095: 2091: 2085: 2082: 2080: 2077: 2075: 2072: 2070: 2067: 2065: 2062: 2060: 2057: 2055: 2052: 2050: 2047: 2045: 2042: 2041: 2039: 2036: 2032: 2026: 2023: 2021: 2018: 2016: 2015:Hawker Hunter 2013: 2011: 2008: 2006: 2003: 2001: 1998: 1996: 1993: 1991: 1988: 1986: 1983: 1981: 1978: 1977: 1975: 1973: 1969: 1965: 1961: 1954: 1949: 1947: 1942: 1940: 1935: 1934: 1931: 1915: 1912: 1910: 1907: 1905: 1902: 1901: 1899: 1895: 1889: 1886: 1884: 1881: 1880: 1878: 1874: 1868: 1865: 1863: 1860: 1859: 1857: 1853: 1847: 1844: 1842: 1839: 1837: 1834: 1832: 1829: 1827: 1824: 1822: 1819: 1817: 1814: 1813: 1811: 1807: 1801: 1798: 1796: 1793: 1791: 1788: 1787: 1785: 1781: 1775: 1772: 1770: 1767: 1765: 1762: 1760: 1757: 1755: 1752: 1751: 1749: 1745: 1739: 1736: 1735: 1733: 1729: 1723: 1722: 1718: 1716: 1715: 1711: 1709: 1708: 1704: 1703: 1701: 1697: 1691: 1688: 1686: 1683: 1681: 1678: 1676: 1673: 1672: 1670: 1666: 1663: 1659: 1653: 1650: 1648: 1645: 1643: 1640: 1638: 1635: 1633: 1630: 1628: 1625: 1623: 1620: 1618: 1615: 1613: 1610: 1608: 1605: 1603: 1600: 1598: 1595: 1593: 1590: 1588: 1585: 1583: 1580: 1578: 1575: 1573: 1570: 1568: 1565: 1563: 1560: 1558: 1555: 1553: 1550: 1548: 1545: 1544: 1542: 1538: 1528: 1525: 1523: 1520: 1518: 1515: 1513: 1510: 1508: 1505: 1503: 1500: 1498: 1495: 1493: 1490: 1488: 1485: 1483: 1480: 1478: 1475: 1473: 1470: 1468: 1465: 1463: 1460: 1458: 1455: 1453: 1450: 1448: 1445: 1443: 1440: 1438: 1435: 1433: 1430: 1428: 1425: 1423: 1420: 1418: 1415: 1413: 1410: 1408: 1405: 1403: 1400: 1398: 1395: 1393: 1390: 1388: 1385: 1383: 1380: 1378: 1375: 1373: 1370: 1368: 1365: 1363: 1360: 1358: 1355: 1353: 1350: 1348: 1345: 1343: 1340: 1338: 1335: 1333: 1330: 1328: 1325: 1323: 1320: 1318: 1315: 1313: 1310: 1308: 1305: 1303: 1300: 1298: 1295: 1293: 1290: 1288: 1285: 1283: 1280: 1278: 1275: 1273: 1270: 1269: 1267: 1263: 1257: 1254: 1252: 1249: 1247: 1244: 1242: 1239: 1237: 1234: 1232: 1229: 1227: 1224: 1222: 1219: 1217: 1214: 1212: 1209: 1207: 1204: 1202: 1199: 1197: 1194: 1193: 1191: 1187: 1184: 1176: 1172: 1165: 1160: 1158: 1153: 1151: 1146: 1145: 1142: 1136: 1133: 1131: 1127: 1124: 1122: 1119: 1116: 1113: 1110: 1107: 1104: 1103:"On the Wing" 1101: 1100: 1090: 1086: 1082: 1081: 1075: 1071: 1069:0-85177-826-7 1065: 1061: 1056: 1052: 1046: 1042: 1037: 1034: 1030: 1026: 1025: 1020: 1016: 1012: 1008: 1003: 1001: 997: 993: 989: 988: 975: 971: 967: 961: 959: 957: 955: 939: 935: 928: 926: 916: 900: 894: 885: 877: 873: 866: 857: 855: 845: 836: 834: 824: 822: 812: 803: 801: 799: 797: 795: 793: 785: 784:Mettam (1970) 780: 771: 769: 767: 760:, p. 45. 759: 754: 745: 743: 741: 739: 729: 727: 725: 723: 713: 711: 706: 691: 688: 687: 686: 685: 684:Related lists 679: 676: 674: 671: 669: 668:Horten Ho 229 666: 665: 664: 663: 651: 648: 645: 644:Wing loading: 642: 639: 636: 633: 630: 627: 624: 621: 618: 617: 616: 614: 606: 602: 598: 595: 592: 591:Gross weight: 589: 586: 585:Empty weight: 583: 580: 578: 574: 571: 568: 565: 562: 559: 556: 553: 550: 547: 544: 541: 538: 537: 536: 534: 529: 528: 524: 520: 517: 509: 498: 495: 494: 491: 480: 479: 473: 471: 467: 462: 460: 456: 451: 447: 442: 440: 439:ejection seat 437: 433: 429: 425: 421: 417: 407: 404: 399: 394: 392: 388: 384: 380: 372: 368: 363: 359: 357: 353: 349: 345: 334: 332: 326: 324: 319: 315: 314:maiden flight 311: 306: 304: 303:trailing edge 300: 296: 292: 287: 284:known as the 283: 273: 271: 267: 262: 260: 256: 252: 248: 244: 240: 235: 233: 229: 225: 221: 220:G. T. R. Hill 217: 213: 209: 194: 192: 187: 183: 179: 175: 174:maiden flight 170: 168: 165: 161: 157: 152: 150: 146: 143:was an early 142: 132: 128: 124: 120: 115: 111: 107: 104: 101: 97: 93: 89: 85: 82: 79: 77: 73: 69: 65: 62: 59: 56: 52: 47: 40: 35: 30: 27: 19: 2715:Flying wings 2601:Saro Skeeter 2518:Auster AOP.9 2513:Auster AOP.6 2445:Short Seamew 2324: 2317:experimental 2300:Short Tucano 2274:Folland Gnat 2172:Avro Lincoln 2096: / 1816:F.K.9/F.K.10 1794: 1783:Experimental 1720: 1713: 1706: 1446: 1182:designations 1178:Manufacturer 1114: 1105: 1078: 1059: 1040: 1022: 1014: 1010: 991: 985:Bibliography 973: 969: 941:. Retrieved 937: 915: 903:. Retrieved 893: 884: 878:(10): 42–46. 875: 871: 865: 844: 811: 779: 753: 683: 682: 661: 660: 649: 643: 637: 631: 625: 619: 612: 610: 596: 590: 584: 575: 569: 563: 557: 551: 545: 539: 532: 530: 526: 522: 518: 515: 514: 463: 450:Warwickshire 443: 413: 395: 375: 352:Fowler flaps 340: 327: 307: 285: 279: 269: 263: 236: 206:Interest in 205: 193:until 1954. 171: 163: 160:jet airliner 153: 140: 138: 122:First flight 109:Number built 99:Primary user 76:Manufacturer 58:Experimental 26: 2573:Helicopters 2415:Heston JC.6 2360:Bristol 188 2296:/Sea Prince 2249:Avro Athena 2177:Avro Vulcan 943:21 November 613:Performance 597:Powerplant: 387:pressurised 247:wind tunnel 216:J. W. Dunne 208:flying wing 197:Development 145:flying wing 61:flying wing 2699:Categories 2460:Short SC.1 2455:Short SB.5 2450:Short SB.3 2430:Saro P.531 2244:Avro Anson 1897:Transports 1572:Argosy (2) 1567:Argosy (1) 1050:0854296972 932:Selig, M. 905:6 December 696:References 570:Wing area: 310:parachutes 202:Background 92:John Lloyd 2500:Transport 2335:BAC TSR-2 1904:Albemarle 1831:Armadillo 1668:Airliners 1582:Armadillo 1552:Albemarle 1180:numerical 1089:0143-5450 1033:0143-5450 872:Aeroplane 701:Citations 558:Wingspan: 546:Capacity: 516:Data from 476:Operators 459:turboprop 348:trim tabs 237:Amid the 2664:EoN Eton 2330:Avro 707 2259:BAE Hawk 2236:Trainers 2037:fighters 1972:Fighters 1846:Starling 1836:Scimitar 1809:Fighters 1699:Airships 1680:Atalanta 1637:Starling 1617:Scimitar 1612:Sea Hawk 1587:Atalanta 657:See also 605:turbojet 371:Coventry 356:spoilers 323:Baginton 295:ailerons 234:engine. 232:turbojet 230:and the 87:Designer 2656:Gliders 2340:BAe EAP 2164:Bombers 2153:(naval) 1883:Tadpole 1800:A.W.171 1774:Whitley 1747:Bombers 1661:By role 1647:Whitley 1642:Tadpole 1540:By name 1527:A.W.690 1522:A.W.681 1517:A.W.680 1512:A.W.670 1507:A.W.660 1502:A.W.650 1497:A.W.171 1492:A.W.169 1487:A.W.168 577:Airfoil 564:Height: 552:Length: 446:Southam 344:rudders 291:elevons 286:A.W.52G 276:A.W.52G 164:A.W.52G 130:Retired 117:History 2094:Strike 1841:Siskin 1821:A.W.16 1795:A.W.52 1769:Sinaia 1764:A.W.29 1759:A.W.23 1754:A.W.19 1690:Apollo 1685:Ensign 1632:Sissit 1627:Sinaia 1622:Siskin 1607:Meteor 1602:Ensign 1557:Apollo 1482:A.W.59 1477:A.W.58 1472:A.W.57 1467:A.W.56 1462:A.W.55 1457:A.W.54 1452:A.W.53 1447:A.W.52 1442:A.W.51 1437:A.W.50 1432:A.W.49 1427:A.W.48 1422:A.W.45 1417:A.W.44 1412:A.W.43 1407:A.W.41 1402:A.W.40 1397:A.W.39 1392:A.W.38 1387:A.W.37 1382:A.W.36 1377:A.W.35 1372:A.W.34 1367:A.W.33 1362:A.W.32 1357:A.W.31 1352:A.W.30 1347:A.W.29 1342:A.W.28 1337:A.W.27 1332:A.W.26 1327:A.W.25 1322:A.W.24 1317:A.W.23 1312:A.W.22 1307:A.W.21 1302:A.W.20 1297:A.W.19 1292:A.W.18 1287:A.W.17 1282:A.W.16 1277:A.W.15 1272:A.W.14 1251:F.K.13 1246:F.K.12 1241:F.K.10 1115:Flight 1106:Flight 1087:  1066:  1047:  1031:  998:  970:Flight 626:Range: 487:  383:tandem 337:A.W.52 282:glider 270:A.W.50 167:glider 32:A.W.52 2035:Naval 1914:Awana 1867:F.K.8 1862:F.K.3 1597:Awana 1592:Atlas 1577:Aries 1256:F.M.4 1236:F.K.9 1231:F.K.8 1226:F.K.7 1221:F.K.6 1216:F.K.5 1211:F.K.4 1206:F.K.3 1201:F.K.2 1196:F.K.1 540:Crew: 299:flaps 18:AW.52 1888:Wolf 1652:Wolf 1547:Ajax 1085:ISSN 1064:ISBN 1045:ISBN 1029:ISSN 996:ISBN 945:2018 907:2022 599:2 × 457:, a 259:drag 139:The 133:1954 54:Type 1826:Ara 1790:Ape 1721:R33 1714:R29 1707:25r 1562:Ara 1128:at 652:1.6 448:in 2701:: 1015:97 1013:, 1009:, 972:. 968:. 953:^ 936:. 924:^ 876:34 874:. 853:^ 832:^ 820:^ 791:^ 765:^ 737:^ 721:^ 709:^ 525:, 521:, 379:μm 369:, 358:. 333:. 305:. 272:. 151:. 1952:e 1945:t 1938:v 1163:e 1156:t 1149:v 1091:. 1072:. 1053:. 1035:. 974:L 947:. 909:. 786:. 579:: 112:2 20:)

Index

AW.52

Experimental
flying wing
Manufacturer
Armstrong Whitworth Aircraft
John Lloyd
Royal Aircraft Establishment
flying wing
Armstrong Whitworth Aircraft
laminar flow airfoil
jet airliner
glider
maiden flight
pitch oscillation
John Oliver Lancaster
emergency ejection
Royal Aircraft Establishment
flying wing
First World War
J. W. Dunne
G. T. R. Hill
Westland-Hill Pterodactyl
laminar flow airfoil
turbojet
Second World War
Ministry of Supply
wind tunnel
National Physical Laboratory
Hawker Hurricane

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