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Wing sweep

Anscombe, A. and Illingworth, L.N. (1952). Wind tunnel observations of boundary layer transition on a wing at various angles of sweep back. ARC R and M 2968. [Pg.303]

Time 2) it is swept (—P). These contradictory requirements are resolved through the invention of variable sweep wing geometry (Exhibit 24.1). [Pg.139]

The AGO specified that no coalition aircraft (fixed or rotary wing) was allowed to enter the TAOR before it was sanitized by a fighter sweep. [Pg.137]

AWACS coverage for flights outside the security zone and complied with that requirement. However, the F-15 pilots involved in the accident, relying on the written guidance in the ACO, believed that no OPC aircraft, fixed or rotary wing, were allowed to enter the TAOR prior to a fighter sweep [5]. [Pg.162]

Main strikes occur between the extremities of the aircraft (wing tips, nose, tail), but they can sweep along the fuselage or across the wing behind projections such as the engines. [Pg.160]

See other pages where Wing sweep is mentioned: [Pg.211]    [Pg.42]    [Pg.105]    [Pg.22]    [Pg.211]    [Pg.42]    [Pg.105]    [Pg.22]    [Pg.41]    [Pg.45]    [Pg.105]    [Pg.109]    [Pg.407]    [Pg.33]    [Pg.65]    [Pg.35]    [Pg.130]    [Pg.88]    [Pg.77]    [Pg.316]    [Pg.314]    [Pg.128]    [Pg.282]    [Pg.85]    [Pg.142]    [Pg.142]    [Pg.15]    [Pg.91]    [Pg.85]    [Pg.3]    [Pg.4]   
See also in sourсe #XX -- [ Pg.21 ]



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