Cover Image

Study of S.T.Ae. formula for load factors (Airplane Section report).

Bibliographic Details
Corporate Author:	United States. Army. Air Corps
Format:	Government Document eBook
Language:	English
Published:	Washington : U.S. GPO, 1925.
Series:	Air Service Info. Circ. Aviation No. 498 McCook Field Rpt. Serial No. 2441
Subjects:	Airplanes, Military. Electronic books.
Online Access:	Connect to the full text of this electronic document

Similar Items

Effect on variation in load factor on structural weight of wings (Airplane Section, S. and A. Branch).
Published: (1922)

Distribution of load among spars in multi-spar construction of airplane wings (Airplane Section report).
Published: (1923)

Study of wing weights (Airplane Section report).
Published: (1925)

Determination of best wing loading for single-seater pursuit airplanes (Airplane Section, S. and A. Branch).
Published: (1922)

Airplane wing fittings (Airplane Section, S. and A. Branch).
Published: (1923)

Strength of wing ribs (Airplane Section report).
Published: (1923)

Report of static test on Engineering Division Messenger airplane (Airplane Section, S. and A. Branch).
Published: (1921)

Report of static test of ski for SE-5 airplane (Airplane Section, S. and A. Branch).
Published: (1922)

Pressure distribution over stabilizer of Vought VE-7 airplane (Airplane Section report).
Published: (1923)

Comparison of structural design requirements for airplanes with loads obtained in full scale pressure distribution tests (Airplane Branch report).
Published: (1932)

Design of internally braced biplane wings (Airplane Section report).
Published: (1923)

Study of stress analysis of JL-6 (Airplane Section, S. and A. Branch).
Published: (1922)

Report of torsional test of Curtiss NBS-4 fuselage (Airplane Section report).
Published: (1925)

Application of method of least work to redundant structures (Airplane Section report).
Published: (1925)

Torsional test of Martin bomber NBS-1 (Airplane Section report).
Published: (1925)

Static proof test of aileron, stabilizer, and elevator of Cox-Heinkel observation airplane P-377 (Airplane Section report).
Published: (1925)

Wind tunnel test of Clark "Y", Clark "Y-15", Clark "Y-18", Clark "Y-21", Gottingen 398, and S.T.Ae.-27a, 6" x 36" airfoils, tests nos. 233, 234, and 237 (Airplane Section report).
Published: (1926)

Report of torsional test of G. Elias NBS-3 fuselage (Airplane Section report).
Published: (1925)

Interference tests on DH4B model and propeller (Airplane Section report).
Published: (1927)

Impact test of JN-4 tail skid and landing chassis (Airplane Section report).
Published: (1923)

Investigation of structural strength of T-2 transport, A.S. numbers 64233 (Airplane Section report).
Published: (1923)

Airplanes and parts : General, propellers considered best for airplanes.
Published: (1926)

Designations of airplanes.
Published: (1918)

Use of airplane brakes.
Published: (1932)

Airplane and parts : O-2 type, control surface tubes.
Published: (1926)

Airplanes and parts : P-1 type, assembly and maintenance instructions.
Published: (1926)

Airplane and parts : O-2 type, replacement of oil lines.
Published: (1926)

Preliminary report on comparison of protective airplane wing coverings.
Published: (1921)

Airplanes and parts : PW-9 type, inner-tripod strut assembly.
Published: (1927)

UO-1 airplane performance.
Published: (1925)

Flying of bi-motor airplanes.
Published: (1918)

Model designation of naval airplanes.
Published: (1932)

Model designation of naval airplanes.
Published: (1928)

DT-2 airplane performance.

Airplane performance and design charts.
Published: (1921)

Model designation of naval airplanes.
Published: (1926)

Model designation of naval airplanes.
Published: (1927)

German airplanes, table of performances.
Published: (1918)

Airplanes on trial, Feb. 1918.
Published: (1918)

Study of horizontal tail surfaces of consolidated XPT-3 (NY-1) (Airplane Branch report).
Published: (1928)