United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory (1917-1958)
Parallel Names
- Langley Aeronautical Laboratory (1917-1958)
Found in 20 Collections and/or Records:
"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.
"Analysis and Prediction of Longitudinal Stability of Airplanes" (NACA Report No. 711), 1941
Document Type: Technical Research Report
Authority: Government Civil (authoritative reference)
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 711, published in 1941.
Scope: NACA research report by R. R. Gilruth and M. D. White.
Contents: See title.
"Analysis of Means of Improving the Uncontrolled Lateral Motions of Personal Airplanes" (NACA Report 1035), 1951
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1035, published in 1951.
Scope: NACA research report by Marion O. McKinney, Jr.
Contents: See title.
"Appreciation and Prediction of Flying Qualities" (NACA Report No. 927), 1949
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 927, published in 1949.
Scope: NACA research report by William H. Phillips.
Contents: See title.
"Calculated Spanwise Lift Distributions, Influence functions, and Influence Coefficients for Unswept Wings In Subsonic Flow" (NACA Report 1228), 1955
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1228, published in 1955.
Scope: NACA research report by Franklin W. Diederich and Martin Zlotnick.
Contents: See title.
"Compressive Strength of Flanges" (NACA Report 1029), 1951
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1029, published in 1951.
Scope: NACA research report by Elbridge Z. Stowell.
Contents: See title.
"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.
"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.