Aerodynamics
Found in 79 Collections and/or Records:
"Experimental Aerodynamic Derivatives of a Sinusoidally Oscillating Air-Foil in Two-Dimensional Flow" (NACA Report 1108), 1952
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1108, published in 1952.
Scope: NACA research report by Robert L. Halfman of the Massachusetts Institute of Technology under NACA contract.
Contents: See title.
"Experiments on Thick Wing Sections" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 3) [Photocopy], 1918-12
"Flow of Air Around a Rotating Cylinder" (Air Service Information Circular Vol. VI, No. 510), 1925-01-07, 1925-06-01
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. VI, No. 510 (dated June 1, 1925), based on McCook Field Report Serial No. 2462 (dated January 7, 1925).
Scope: Airplane Section report prepared by E.N. Fales, Engineering Division, Air Service, McCook Field, Dayton, Ohio.
Contents: See title.
"Force- and Pressure-Distrubution Measurements on Eight Fuselages" [Translation of paper titled "Kraftmessungen und Druckverteilungsmessungen an 8 Rümpfen" by G. Lange] (NACA Technical Memorandum No. 1194), 1941-10-24, 1948-10
"Full-Scale Tunnel Investigation of the Control and Stability of A Twin-Engine Monoplane with Propellers Operating" [Originally published as an Advance Restricted Report in November 1942] (NACA Wartime Report L-425), 1942-11, Circa late 1945 to 1946
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Wartime Report L-425, published soon after the end of WW II. Originally published as an Advance Restricted Report in November 1942.
Scope: NACA research report by Harold H. Sweberg.
Contents: See title.
"High-Speed Tests of A Model Twin-Engine Low-Wing Transport Airplane" (NACA Report No. 750), 1942
Document Type: Technical Research Report
Authority: Government Civil (authoritative reference)
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 750, published in 1942.
Scope: NACA research report by John V. Becker and Lloyd H. Leonard.
Contents: See title.
"Horizontal Tail Loads in Maneuvering Flight" (NACA Report 1007), 1951
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1007, published in 1951.
Scope: NACA research report by Henry A. Pearson, William A. McGowan, and James J. Donegan.
Contents: See title.
"Instruction sur le Calcul des Performances" (Second Edition, Octobre 1928) [Instruction for the Calculation of Performances], 1928-10
Document Type: Technical Reference Handbook
Authority: Government Civil (authoritative reference)
Scope & Contents: early work on calculating aeronautical performance by the French government equivalent of the U.S. National Advisory Committee for Aeronautics (NACA).
"Interference Effects of Single and Multiple Round or Slotted Jets on a VTOL Model in Transition" (NASA Technical Note TN D-2380), 1964-08
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2380, dated August 1964.
Scope: Preliminary NASA research report by Raymond D. Vogler of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Investigation in the Langley 19-Foot Pressure Tunnel of Two Wings of NACA 65-210 and 64-210 Airfoil Sections with Various Type Flaps" (NACA Report No. 942), 1949
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 942, published in 1949.
Scope: NACA research report by James C. Sivells and Stanley H. Spooner.
Contents: See title.