Effects of variations in specificity of knowledge of results on the improvement of a perceptual skill /

Prepared under Project no. 1710, Task no. 71605."August 1960."Mode of access: Internet

Time-dependent, elasto-plastic bending analysis for structures under arbitrary load-temperature environments.

"April 1960."Includes bibliographical references (page 38).Research supported by the United States Air Force Air Research and Development Command, and performed by The Martin Company under Flight Dynamics Laboratory contract no.Mode of access: Internet

Liquid oxygen converter /

"Contract no. AF 33(616)--6756, project no. 6373, task no. 63120.""Report No. ARF 3164-12""October 1960."Includes bibliography, (pages 32-37).Mode of access: Internet

Sampled-data deviations in a vertical indicator with a stellar monitor /

"Prepared under Task no. 110-A.""September 1960."Includes bibliographical references (pages 62-65).Mode of access: Internet

Guide to aircrew personal and aircraft installed equipment /

Prepared by Wright Air Development Division, Operational Support Engineering Division, under Project No. 6325."September 1960.""WADD Technical Note 60-230.""(Supersedes WADC TN 58-259, Dated August 1958)."Mode of access: Internet

Flight control study of a manned re-entry vehicle /

"Project No. 8225, Task No. 82182.""July 1960."U.S. Air Force Contract No.Mode of access: Internet

Considerations and recommendations for developing a materials information processing capability /

"Project No. 7381.""February 1961."Includes bibliographical references (pages 10-12).Print reproduction.U.S. Air Force Contract No.Mode of access: Internet

Telemetry transducer handbook.

"Project No. 4107, Task No. 82251.""28 April 1961."U.S. Air Force Contract No.Mode of access: Internet

Human factors in design of automatic programming and recording for trainers (AN/ASG-15 TI fire control system trainer) /

"August 1960."Includes bibliographical references.Mode of access: Internet

Time-dependent, elasto-plastic bending analysis for structures under arbitrary load-temperature environments.

"April 1960."Includes bibliographical references (page 64).Research supported by the United States Air Force Air Research and Development Command, and performed by The Martin Company under Flight Dynamics Laboratory contract no.Mode of access: Internet