Cover Image

Technical Bulletin No. 40 : Development of military aircraft material for U.S. Air Service under supervision of Engineering Division.

Bibliographic Details
Corporate Author:	United States. Army. Air Corps
Format:	Government Document eBook
Language:	English
Published:	McCook Field, Ohio : [publisher not identified], 1924.
Series:	Air Service Info. Circ. Aviation No. 481 Air Service Tech. Bull. No. 40
Subjects:	Airplanes, Military. Engines. Motors. Electronic books.
Online Access:	Connect to the full text of this electronic document

Similar Items

Air-cooled engines in naval aircraft.
Published: (1930)

Short technical descriptions, airplanes in use and on order by American E.F.
Published: (1918)

Amendment to Technical Note No. 96, Series of 1930; Non-interchangeability of carburetors.
Published: (1931)

Amendment to Technical Note No. 82, Series of 1930; Service information for overhaul of Eclipse starters and generators.
Published: (1932)

Power plants for aircraft.
Published: (1930)

Aircraft engine spark plugs.
Published: (1924)

Care and maintenance of Scintilla aircraft magnetos.
Published: (1930)

Reconditioning of aircraft engine spark plugs.
Published: (1932)

Curtiss D-12 aircraft engine handbook.
Published: (1930)

Method used by Engineering Division of Air Service for computing horsepower available from engine with 2-bladed wood propeller (Airplane Section report).
Published: (1925)

Recent developments in aircraft ignition (Power Plant Branch report).
Published: (1928)

Vibration characteristics of aircraft engine crank shafts (Power Plant Branch report).
Published: (1932)

Performance test on Engineering Division CO-5 airplane equipped with Liberty "12" engine.
Published: (1924)

Test of supercharger air coolers (Power Plant Section report).
Published: (1923)

First 50-hour test of air-cooled Liberty engine.
Published: (1926)

Clogging of fuel strainers (Material Section report).
Published: (1925)

Comparative effect on engine operation in flight of outside and inside air intakes.
Published: (1921)

Instructions, Leece-Neville voltage regulated electrical generating equipment for aircraft engines, 12-15 volt engine driven generators, types E-3, E-4.
Published: (1931)

Official performance test of Engineering Division CO-5 equipped with 12-cylinder Liberty engine (Flying Section report).
Published: (1925)

Official performance test of Engineering Division XCO-6 equipped with "12" cylinder inverted Liberty engine (Flying Section report).
Published: (1925)

Tests of back-suction and air-bleed type mixture controls in flight (Power Plant Section report).
Published: (1922)

First full throttle endurance test of Liberty engine, equipped with various experimental materials (Power Plant Section report).
Published: (1925)

Performance estimate of Pomilio FVL-8 equipped with 8-cylinder Liberty engine; estimated by means of "airplane performance and design charts," as outlined in Air Service Information Circular, Vol. II, No. 183.
Published: (1921)

Performance estimate of Lepere G. H. 11 equipped with 400 h.p. Liberty "12" engine, estimated by means of "airplane performance and design charts" as outlined in Air Service Information Circular, Vol. II, No. 183.
Published: (1921)

Care, overhaul, and operation of Lawrance J-1 engine.
Published: (1924)

Stress analysis of model W-1 engine (Power Plant Section report).
Published: (1924)

Official performance test of Boeing pursuit PW-9 equipped with Curtiss D-12 high compression engine (Flying Section report).
Published: (1924)

Performance test of Boeing pursuit, type I, equipped with Curtiss D-12 engine.
Published: (1924)

Performance test on Fokker CO-4 equipped with Liberty "12" engine and side radiators.
Published: (1924)

Economy test of DH-4 (Flying Section report).
Published: (1924)

Bellows (Sylphon) fuel pump for Liberty "12" and Wright "H" engines (Power Plant Section report).
Published: (1924)

Performance test on Fokker CO-4 equipped with Liberty "12" engine and nose radiators.
Published: (1924)

Comparison tests of storage preparations for aviation engine storage of less than 6 months (Power Plant Section report).
Published: (1924)

Performance test of G. Elias TA-1, type XIV, equipped with Lawrance R-9 engine.
Published: (1923)

Sediment deposit in carburetors.
Published: (1922)

Test of Zenith carburetor, model U.S. 52, fitted with "plain tube" and Britton type discharge nozzles (Power Plant Section report).
Published: (1922)

Standard engine test of Curtiss D-12 high and low compression engines (Power Plant Section report).
Published: (1926)

Standard engine report on Curtiss 12-cylinder model C-12, geared aviation engine, rated at 400 h.p. at 2,250 revolutions per minute (engine speed) (Power Plant Section report).
Published: (1922)

Performance of Packard model 1A-1116 aviation engine with 6 : 1 compression ratio.
Published: (1921)

Official performance test of Douglas XO-2 equipped with Liberty "12" engine and standard steel propeller set at 18 degrees (Flying Section report).
Published: (1925)