Precise formulas for restrained beam with axial load of compression, and with one restraining moment known (airplane branch report)

Metadata Field	Value	Language
dc.date.accessioned	2017-09-09T16:55:53Z
dc.date.available	2017-09-09T16:55:53Z
dc.date.created	1929-08-01	en_US
dc.identifier.uri	http://hdl.handle.net/11200/48949
dc.description	Cases of axially loaded beams with two supports, restraining moments at both supports, and one restraining moment determined by loads outside the support or by the type of support, are sometimes encountered in airplane structures. The formulas for computing the unknown restraining moment are herein derived for four cases of side load. These formulas are supplementary to the "Precise formulas" given in Airplane Design, by A. S. Niles, chapter 2, or in Air Corps Information Circular No. 493, Section I.	en_US
dc.format	PDF	en_US
dc.publisher	Washington, D.C. : Chief of Air Corps	en_US
dc.relation.ispartofseries	Air Corps information circular (Aviation) ; v. 7, no. 624	en_US
dc.relation.ispartofseries	Air Corps technical report ; Serial no. 2899	en_US
dc.subject	Aeronautics--Research	en_US
dc.subject	Aeronautics--Systems engineering	en_US
dc.subject	Mathematics--Formulae	en_US
dc.subject	Airplanes--Design and construction	en_US
dc.title	Precise formulas for restrained beam with axial load of compression, and with one restraining moment known (airplane branch report)	en_US
dc.type	Text	en_US

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