Show simple item record

dc.creatorOber, Shatswellen_US
dc.creatorMarkham, John R.en_US
dc.date.accessioned2017-07-20T19:31:13Zen_US
dc.date.available2017-07-20T19:31:13Zen_US
dc.date.created1927-02-01en_US
dc.identifier.urihttp://hdl.handle.net/11200/48913
dc.descriptionContinuing the series of mutual interference and slipstream tests in the Massachusetts Institute of Technology 7 1/2-foot tunnel, described in the report "Preliminary tests of DH4B model and Propeller", experiments have been completed for several angles of attack, and some work has been done on the effects due to changes in stabilizer angle, removing various parts, etc. This report gives the results of all tests which are finished, but must not be considered final, in particular in regard to propeller torque. The same one-fourth scale model of a DH4B was used throughout.en_US
dc.formatPDFen_US
dc.publisherWashington, D.C. : Chief of the Air Corpsen_US
dc.relation.ispartofseriesAir Corps information circular (Aviation) ; v. 6, no. 582en_US
dc.relation.ispartofseriesMateriel Division report ; Serial no. 2699en_US
dc.subjectBiplanesen_US
dc.subjectAirplanes--Models--Aerodynamicsen_US
dc.subjectWind tunnel testingen_US
dc.subjectAirplanes--Design and constructionen_US
dc.subjectAeronautics--Systems engineeringen_US
dc.subjectAeronautics--Researchen_US
dc.subjectPropellers, Aerialen_US
dc.titleInterference tests on DH4B model and propeller (airplane section report)en_US
dc.typeTexten_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record