Correspondence from George Walter Chamberlain, 1942

Letters in which Chamberlain recalls his experiences relating to Native Americans in Maine and his research in the Massachusetts State Archives about this subject. These were digitized from box 1, folder 21 of the Fannie Hardy Eckstorm Papers. Documents from this folder that did not pertain to Native Americans in Maine were not scanned and are not included in this filehttps://digitalcommons.library.umaine.edu/eckstorm_papers/1005/thumbnail.jp

Vital Records of Lebanon, Maine, To the Year 1892 - Volume I - Births

Records of Lebanon, Maine, To the Year 1892 - Volume I - Births George Walter Chamberlain, M.S., Editor; William Davis Patterson & Alfred Johnson, Committee on Publication. Published Under Authority of the Maine Historical Society, 1922. Wright & Potter Printing Company, 32 Derne Street, Boston, Mass. Lebanon Births To the Year 1892.https://digitalcommons.usm.maine.edu/me_collection/1141/thumbnail.jp

Vital Records of Lebanon, Maine, To the Year 1892 - Volume III - Deaths

Vital Records of Lebanon, Maine, To the Year 1892 - Volume III - Deaths George Walter Chamberlain, M.S., Editor; William Davis Patterson & Alfred Johnson, Committee on Publication. Published Under Authority of the Maine Historical Society, 1923. T.R. Marvin & Son, Printers, 152 Purchase Street, Boston, Mass. Lebanon Deaths To the Year 1892.https://digitalcommons.usm.maine.edu/me_collection/1139/thumbnail.jp

Vital Records of Lebanon, Maine, To the Year 1892 - Volume II - Marriages

Vital Records of Lebanon, Maine, To the Year 1892 - Volume II - Marriages George Walter Chamberlain, M.S., Editor; William Davis Patterson & Alfred Johnson, Committee on Publication. Published Under Authority of the Maine Historical Society, 1922. T.R. Marvin & Son, Printers, 152 Purchase Street, Boston, Mass. Lebanon Marriages To the Year 1892.https://digitalcommons.usm.maine.edu/me_collection/1140/thumbnail.jp

Aerodynamic coefficients of a symmetrical airfoil in an oscillating flow

A symmetrical airfoil at fixed angle of attack from 0 to 35 degrees was placed in an air flow with controlled velocity oscillations at 10 Hz. The instantaneous pressure distribution and flow velocity were measured simultaneously. Pressure information was integrated numerically to determine instantaneous values for lift, drag and moment about the quarter chord. The results were plotted as three-dimensional surface plots in angle of attack, cycle time and performance coefficient axes, or with chordwise position, cycle time and pressure coefficient axes, as appropriate. The pressure distribution over the airfoil was shown to be primarily a function of freestream static pressure. Aerodynamic coefficients as a function of angle of attack and time exhibited seemingly random, erratic behavior, whereas the mean values of the same coefficients were similar in nature to those obtained in steady flow. The data indicate that the instantaneous performance of an airfoil in an oscillating flow is not merely a continuum of many quasi-steady states.http://archive.org/details/aerodynamiccoeff1094510801Lieutenant, United States NavyApproved for public release; distribution is unlimited

Construction Contractors\u27 Audit Manual, Volume 1

https://egrove.olemiss.edu/aicpa_guides/2174/thumbnail.jp

Construction Contractors\u27 Audit Manual, Volume 2

https://egrove.olemiss.edu/aicpa_guides/2175/thumbnail.jp