Cantilever monoplane, with 45-m. wing span; 2400 hp. developed by four Junkers L88 750-hp. engines; design is step toward flying wing; propellers, placed in front of leading edge by streamlined fairing receive power from engines by means of long transmission shafts; thickness of wing at socket exceeds 2 m. so that comfortable cabins can be arranged. (see also English description in Flight, vol. 21, no. 48, Nov. 29, 1929, p. 1264, 3 figs.; and Aero Digest, vol. 15, no. 6, Dec. 1929, p. 170, 1 fig.)
Tendency toward flying wing; the Junkers G38
Vers l'aile volante: le Junkers G 38
Aeronautique ; 11 , n 127
1929
3 Figs.
Article (Journal)
French
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Tendency toward flying wing; the Junkers G38
Engineering Index Backfile | 1929
Tendency toward flying wing; the Junkers G38
Engineering Index Backfile | 1929
Engineering Index Backfile | 1937
|Engineering Index Backfile | 1935
|Emerald Group Publishing | 1937
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