Airplanes -- Design and construction -- Research
Found in 125 Collections and/or Records:
"A Comparison of the Results from General Tank Tests of 1/6- and 1/12-Full Size Models of the British Singapore IIC Flying Boat" (NACA Technical Notes No. 858), 1942-08
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NACA Technical Note 858, dated August 1942.
Scope: Preliminary NACA research report by Starr Truscott and John R. Dawson of Langley Memorial Aeronautical Laboratory, Langley Field, Va.
Contents: See title.
"A Semiempirical Procedure for Computing the Water-Pressure Distrubution on Flat and V-Bottom Prismatic Surfaces During Impact or Planing" (NACA Technical Note 2583), 1951-12
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NACA Technical Note 2583, dated December 1951.
Scope: Preliminary NACA research report by Robert F. Smiley of Langley Aeronautical Laboratory, Langley Field, Va.
Contents: See title.
"A Study of Controllability, Angular Velocity, and Dynamic Stability of an Airplane about the Axis of Pitch" (Air Service Information Circular (Aviation) Vol. V, No. 418), 1922-08-19, 1923-04-01
"Aerodynamic Characteristics of a 4-Engine Monoplane Showing Comparison of Air-Cooled and Liquid-Cooled Engine Installations" [Originally published as an Advance Confidential Report in July 1939] (NACA Wartime Report L-471), 1939-07, 1947-05-05
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Wartime Report L-471, published soon after the end of WW II. Originally published as an Advance Confidential Report in July 1939.
Scope: NACA research report by Abe Silverstein and Herbert A. Wilson, Jr.
Contents: See title.
"Aerodynamic Characteristics of A Full-Scale Propeller Tested with both Rigid and Flapping Blades and with Cyclic Pitch Control" (NASA Technical Note TN D-1774), 1963-05
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-1774, dated May 1963.
Scope: Preliminary NASA research report by Kenneth W. Mort and Paul F. Yaggy of Ames Research Center, Moffett Field, Calif.
Contents: See title
"Aerodynamic Characteristics of a Large-Scale Model with Two High Disk-Loading Fans Mounted in the Wing" (NASA Technical Note TN D-1650), 1963-02
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-1650, dated February, 1963.
Scope: Preliminary NASA research report by David H. Hickey and Leo P. Hall of Ames Research Center, Moffett Field, Calif.
Contents: See title
"Aerodynamic Data On Large Semispan Tilting Wing with 0.6-Diameter Chord, Single Slotted Flap, and Single Propeller Rotating Up at Tip" (NASA Technical Note TN D-1586), 1964-10
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-1586, dated October 1964.
Scope: Preliminary NASA research report by Marvin P. Fink, Robert G. Mitchell and Lucy C. White of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Aerodynamic Effects of Modifiying Wing Inbord Trailing-Edge Camber of a Model at High Subsonic Speeds" (NASA Technical Note TN D-1809), 1963-05
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-1809, dated May 1963.
Scope: Preliminary NASA research report by Richard J. Re of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Aileron Effectiveness: Wind Tunnel Tests of U.S.A.-35 (Half-Span) Airfoil with Skewed Ailerons" (Air Service Information Circular (Aviation) Vol. V, No. 454), 1923-11-05, 1924-03-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. V, No. 454 (dated March 15, 1924), based on McCook Field Report Serial No. 2252 (dated November 5, 1923).
Scope: Airplane Section report prepared by A.L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.
Contents: See title.
"Aileron Effectiveness: Wind Tunnel Tests of U.S.A.-35 (Half-Span) Airfoil with Skewed Ailerons" (Air Service Information Circular (Aviation) Vol. V, No. 454), 1923-11-05, 1924-03-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. V, No. 454 (dated March 15, 1924), based on McCook Field Report Serial No. 2252 (dated November 5, 1923).
Scope: Airplane Section report prepared by A.L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.
Contents: See title.