... at the fuselage - ground contact line ( fig . 23 ( c ) ) . Most ignition sources in ... landing light ( e ) ( f ) Right light Ship # 972 ( e ) Landing - light ... filament ignited the fuel spilled within the wing within 0.35 second after ...
Experimental and Predicted Longitudinal and Lateral-directional Response Characteristics of a Large Flexible 35̊ Swept-wing Airplane at an Altitude of 35,000 Feet
... A / A2 , blade speed parameter The relation among Ular 1 , and stator exit flow angle a3 . 1.0 Rotor entrance Mach ... A / A2 such as might occur during turbine manufacture , the manu- A , OM1.3 can be used to estimate facturing - error ...
This website uses cookies and collects data for optimal performance. Your continued use signifies agreement to our Privacy Policy.