The Short "Scion Senior" commercial airplane (British), A Four-engine high-wing cantilever monoplane.

The Short "Scion Senior" commercial airplane (British) : a four-engine high-wing cantilever monoplane.
Published: (1935)

Market for commercial airplanes in Yunnan Province, China.
Published: (1920)

Effect of slipstream on airplane wing.
Published: (1939)

The Lat©♭co©·re 521 "Lieutenant de vaisseau Paris" commercial flying boat (French), A Two-deck Six-engine semicantilever sesquiplane.
Published: (1936)

Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails : 1. Basic loading condition.
Published: (1937)

The design of airplane-engine superchargers.
Published: (1937)

Forces and moments on airplane engine mounts.
Published: (1936)

Way to increased airplane engine power.
Published: (1939)

An approximate spin design criterion for monoplanes.
Published: (1939)

Engines and propellers for powered gliders and light airplanes.
Published: (1938)

Estonian government to purchase light airplanes.
Published: (1928)

Calculation of natural frequency of cantilever monoplane wing (Airplane Branch report).
Published: (1930)

Airplane dopes used by German aircraft manufacturers.
Published: (1928)

Some aspects of stalling of modern low℗--wing monoplanes.
Published: (1938)

Early airplanes /
by: Blake, John
Published: (1974)

Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails : 2. Mass distributed along fuselage.
Published: (1937)

Effect of changes in tail arrangement upon spinning of low-wing monoplane model.
Published: (1936)

Spinning characteristics of wings : 5, N. A. C. A. 0009, 23018, and 6718 monoplane wings.
Published: (1938)

Fairey "Battle" medium bomber airplane (British), An all-metal low℗--wing cantilever monoplane.
Published: (1937)

Aircraft Circulars : Armstrong Whitworth 27 "Ensign" commercial airplane (British), An all-metal high-wing monoplane.
Published: (1937)

Cooling of airplane engines at low air speeds.
Published: (1936)

Free℗--spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails : 4, Effect of center-of℗--gravity location.
Published: (1939)

Notes on technique of landing airplanes equipped with wing flaps.
Published: (1936)

Some aspects of torsion in multispar cantilever wings (Airplane Branch report).
Published: (1929)

Contribution to aerodynamics of rotating-wing aircraft.
Published: (1939)

Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, III. Mass distributed along the wings.
Published: (1938)

The formation of ice on airplanes.
Published: (1936)

Analysis of 2-spar cantilever wings with special reference to torsion and load transference.
Published: (1934)

Performance test of Loening monoplane with 300 h.p. Hispano-Suiza engine.
Published: (1920)

Engine performance and knock rating of fuels for high℗-out-put aircraft engines.
Published: (1938)

Pilots' Powerplant Manaul.
Published: (1940)

Charts for calculating performance of airplanes having constant-speed propellers.
Published: (1936)

The Airspeed "Oxford" training airplane (British), A two-engine cantilever monoplane.
Published: (1937)

Weight estimate of cantilever monoplane wings of corrugated aluminum alloy box-type construction for pursuit, attack, twin-engined observation, and transport airplanes (Airplane Branch report).
Published: (1931)

The pressure available for ground cooling in front of cowling of air-cooled airplane engines.
Published: (1938)

Occupations related to airplane woodworker.
Published: (1943)