Airplanes -- Control systems
Found in 20 Collections and/or Records:
"Memorandum on Comparative Effectiveness and Efficiency of Ailerons and Interplane Flaps, and of Broad and Shallow Ailerons" (Bureau of Aeronautics Technical Note No. 5) [Photocopy], 1923
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Navy Department, Bureau of Aeronautics Technical Note No. 5 (dated 1923), based on "Reprint of Navy Department, Bureau of Construction and Repair A. T. N. [Aeronautical Technical Note] No. 8)".
Scope: Report #40477-23 prepared by Alexander Klemin.
Contents: See title.
"Method for Calculating the Rolling and Yawing Moments due to Rolling for Unswept Wings With or Without Flaps or Ailerons By Use of Nonlinear Section Lift Data" (NACA Report 1167), 1954
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1167, published in 1954.
Scope: NACA research report by Albert P. Martina.
Contents: See title.
"Report of Control Cable Guide Running Test" (Air Service Information Circular (Heavier-Than-Air) Vol. II, No. 110), 1920-07-26, 1920-09-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Heavier-than-Air) Vol. II, No. 110 (dated September 15, 1920). Prepared from McCook Field Report Serial No. 1332, dated July 26, 1920 and Materia Section Report No. 96.
Scope: Report prepared by Material Section, Engineering Division, Air Service, McCook Field.
Contents: See title.
"Review of Propeller-Rotor Whirl Flutter" (NASA Technical Report TR R-264), 1967-07
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Report TR R-264, dated July, 1967.
Scope: NASA research report by Wilmer H. Reed III of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Stabilizer and Elevator Pressure Distribution" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 3) [Photocopy], 1918-12
"Summary of Section Data on Trailing-Edge High-Lift Devices (NACA Report No. 938), 1949
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 938, published in 1949.
Scope: NACA research report by Jones F. Cahill.
Contents: See title.
"Test Report of Kellogg 600-Watt Reverse Current Relay" (Air Service Information Circular (Aviation) Vol. II, No. 189), 1920-10-25, 1921-03-20
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. II, No. 189 (dated March 20, 1921), based on McCook Field Report Serial No. 1429, dated October 25, 1920).
Scope: Report prepared by Equipment Section, Engineering Division, Air Service, McCook Field.
Contents: See title.
"The Effectiveness at High Subsonic Mach Numbers of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil Section" (NACA Technical Note 3127), 1954-03
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NACA Technical Note 3127, dated March 1954.
Scope: Preliminary NACA research report by Louis S. Stivers, Jr. of Ames Aeronautical Laboratory, Moffett Field, Calif.
Contents: See title.