History of aicraft piston engines

3 1 1936 p p 3 41 350 illus drgs diagrs w ood d onald

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: of r adial engines; e xperince of S tearman A ircraft C o. B EISEL, R E X B ., M ACCLAIN, A . L., and T HOMAS, F . M. T h e cowling and cooling of radial e ngines. Journal of the Royal Aeronautical Society ( July 1934), vol. 38, pp. 6 13-650, i llus., d iagrs., graph data. Orginally given as a p aper before ASME 1934 a nnual m eeting. 117 K EMPER, C . Fin and baffle design for a ir-cooled engines. SAE Transactions, v ol. 29, 1934, p p. 3 70-376. Summary of w ork b y N ACA. N ORTH, J . D. E ngine cowling. Journal of the Royal Aeronautical Society ( July 1934), vol. 3 8, p p. 5 66-612, illus., diagrs., graph data. Broad historical treatment. S HOEMAKER, J . M., R HINES, T . B., and S ARGENT, H . H., J R . F urther progress in controlled c ooling of r adial engines. SAE Transactions, v ol. 30, 1935, pp. 3 49-360, illus., d iagrs., graph data. Relates t o cowl flaps. D ucted radiators for a ero-engines. Interavia, n o. 357 ( September 3 , 1936), p p. 1-3. A NDERSON, P . A. A ir-cooled radial aircraft engine installation. SAE Transactions, v ol. 3 1, 1936, p p. 3 41-350, illus., drgs., diagrs. W OOD, D ONALD H . E ngine nacelles a nd p ropellers a nd a irplane performance. SAE Transactions, vol. 38, 1936, p p. 1 48-160, illus., drgs., diagrs., t ab. and g raph data. B EISEL, R E X B. Why use cowl flaps? Journal of the Aeronautical Sciences, v ol. 4 , no. 5 (May 1937), p p. 1 85-191, illus. C AMPBELL, K ENNETH. C ylinder cooling a nd d rag of r adial engine installations. SAE Transactions, v ol. 33, 1938, p p . 5 15-528, illus., drgs., graph data. Relates t o c owlings, cowl flaps, a nd baffle designs. L EE, JOHN G . A ir-cooled vs. l iquid-cooled aircraft. Journal of the Aeronautical Sciences, vol. 8, no. 6 (April 1941), p p. 2 19-229, illus., diagrs., graph data. R ICKERT, P ., and H ELD, A . H eat transfer in g eometrically similar cylinders. NACA Technical Memorandum, n o. 977, 1941, 11 p p., g raph data, bibl. of 3 i tems. Also see a rticles i n the following NACA Reports: 4th, 1918; 5th, 1919; 6th, 1920; 13th, 1927; 15th, 1929; 21st, 1935; 23rd, 1937; 24th, 1938; 25th, 1939. Carburetors, Carburetion, and Fuel Injection D evelopment of S tromberg carburetors. Aviation, vol. 23, no. 5 ( August 1, 1927), p . 247. W ILLGOOS, A . V. D. P ratt a nd W hitney fuel injection system. U.S. Air Services, v ol. 17, N o. 2 ( February 1932), p p. 3 5-36. C LOTHIER, W . C. Ice f ormation in c arburetors. Journal of the Royal Aeronautical Society ( September 1935), vol. 39, pp. 7 61-806, diagrs., graph data. P ratt & W hitney automatic power a nd m ixture control. Aero Digest, v ol. 26, no. 1 ( July 1935), p p. 3 8-40, 4 2. A utomatic mixture: N ew P ratt & W hitney carburetor control gets long workout o n first P an American flight. Aviation, vol. 34, no. 6 ( June 1935), p p. 3 5-36. B EARDSLEY, G UY E . An a utomatic power a nd m ixture control for a ircraft engines. SAE Transactions, vol. 37, 1935, p p. 3 01-306, illus., diagrs., graph data. A utomatic power a nd m ixtur...
View Full Document

This document was uploaded on 01/19/2014.

Ask a homework question - tutors are online