dc.contributor.author | Project Whirlwind Research Staff | en_US |
dc.date.accessioned | 2009-06-15T21:24:32Z | |
dc.date.available | 2009-06-15T21:24:32Z | |
dc.date.issued | 2009-06-15T21:24:32Z | |
dc.identifier | MC665_r17_sr-2-v-3.pdf | en_US |
dc.identifier.uri | http://hdl.handle.net/1721.3/40678 | |
dc.description | Includes: summary, origin and purpose of the project, present status, aerodynamic equations, dynamic range and accuracy, non-linear coefficients, analogue circuits, wind tunnel tests, cockpit design, and appendices. | en_US |
dc.description | Includes: figures, block diagrams, drawings, and charts. | en_US |
dc.description.abstract | Reprint of an in-depth review of Project Whirlwind in the April of 1946. | en_US |
dc.language.iso | en | en_US |
dc.publisher | MIT Servomechanisms Laboratory | en_US |
dc.relation.ispartofseries | MIT DIC 6345 | en_US |
dc.relation.ispartofseries | Project Whirlwind Summary Report SR-2-v-3 | en_US |
dc.relation.ispartofseries | Project Whirlwind Collection, MC665 | en_US |
dc.subject.other | flight trainers | en_US |
dc.subject.other | aircraft analyser | en_US |
dc.subject.other | motion equations | en_US |
dc.subject.other | pilot reaction | en_US |
dc.subject.other | automatically controlled flight | en_US |
dc.subject.other | analog computing | en_US |
dc.subject.other | digital computation | en_US |
dc.subject.other | system of axes | en_US |
dc.subject.other | landing and take-off equations | en_US |
dc.subject.other | stall conditions | en_US |
dc.subject.other | control forces | en_US |
dc.subject.other | engine simulation | en_US |
dc.subject.other | pitching angular velocity | en_US |
dc.subject.other | aircraft safety | en_US |
dc.subject.other | electrical signal range | en_US |
dc.subject.other | analog operating range | en_US |
dc.subject.other | voltage carrier | en_US |
dc.subject.other | control force equipment | en_US |
dc.title | Summary report no. 2, volume 3, reprint of summary report no. 1 | en_US |
dc.type | Technical Report | en_US |