By Jim Mesko
The Squadron sign courses "In motion" books supply fans, historians and modelers with awesome photographic insurance over quite a lot of chosen topics. pictures are drawn from many inner most collections and files to depict the identify characteristic in its historic atmosphere. additionally, every one quantity positive aspects unique disguise artwork, complete colour profiles, certain scale drawings, scrap paintings and crucial descriptive textual content to convey those histories to existence. study all concerning the Douglas A-26 Invader which was once a usa twin-engine gentle bomber and assault plane outfitted by means of Douglas airplane in the course of international battle II that still observed carrier in the course of a number of of the chilly War's significant conflicts. Douglas begun the A-26 in 1941. The Douglas A-26 (now referred to as the B-26) bomber used to be the single American bomber to fly missions in 3 wars. After global conflict II, it served as a first-line bomber in the course of the Korean struggle and through the Vietnam battle. The final U.S. army Invader used to be retired in 1972 and donated to the Smithsonian's nationwide Air and area Museum.
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K, "Laminar Flame Speeds of Hydrocarbon and Air Mixture with Hydrogen Addition," Combustion and Flame, Vol. 86, 1986, pp. 337-347. 12 Kim, Y. , "Propagation and Extinction of a Flame in a Stagnation-Point Flow," Combustion and Flame, Vol. 73, 1988, pp. 303-313. Near-Field CARS Measurements and the Local Extinction of TYirbulent Jet Diffusion Flames Fumiaki Takahashi* and Marlin D. Vangsnesst University of Dayton, Dayton, Ohio 45469 Abstract Local extinction and subsequent lifting mechanisms have been investigated in turbulent jet diffusion flames of methane stabilized on a thick-walled fuel tube in coflowing air.
0°/o Fig. 4 Typical mean velocity profile along the stagnation streamline. ST Oooo°°7 10 0 10 y(mm) 20 CHARACTERISTICS OF TURBULENT PREMIXED FLAME 31 / A AA 6 A ", *•• ' 5 . 3 2 1 Fig. , Stagnation flame, ClU/Air Chengg and Ng, V-flame, C 2 H*/Air 5 Turbulent flame speed compared with that of other workers. mean stretch rate of the approach flow is defined from the velocity gradient of the linear velocity profile as shown in Fig. 4. 2'8'10 Particularly, our results agree well with those of Liu and Lenze8 obtained from stagnation flame.
H. Non-Steady Flame Propagation, AGARDograph no. 75, MacMillian, New York, 1964. , "The Mechanism of Transition from Deflagration to Detonation," Progress in Combustion Science, Vol. 6, 1980, pp. 369-389. , "Theory of Vorticity Generation by Shock Waves and Flame Interactions," Progress in Astronautics and Aeronautics, Vol. 94, AIAA, New York, 1984, pp. 429448. H. Hirschel, Friedr. Vieweg und Sohn, Braun- schweig/Wiesbaden, Germany, 1985, pp. 56-70. , "Numerical Analaysis of Flowfields Generated by Accelerating Flames," AIAA Journal, Vol.
A-26 Invader in Action by Jim Mesko