Aerodynamics
Found in 94 Collections and/or Records:
Airplane Aerodynamics, 1951
"An Analyisis of the Effect of Lift-Drag Ratio and Stalling Speed On Landing-Flare Characteristics" (NACA Technical Note 1930), 1949-09
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NACA Technical Note 1930, dated September 1949.
Scope: Preliminary NACA research report by J. Calvin Lovell and Stanley Lipson of Langley Memorial Aeronautical Laboratory, Langley Field, Va.
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.
"Appendix to Air Service Information Circular (Aviation) Vol V, No. 455: Wind Tunnel Test of the Original TA-4 with the Following Airfoils: USA-27C Large; USA-27C Small; Gottingen 387; Gottingen 255" (Air Service Information Circular (Aviation) Vol. V, No. 455 (Appendix), 1924-04-29, 1924-08-01
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. V, No. 455 (Appendix) (August 1, 1924), based on McCook Field Report Serial No. 2331 (dated April 29, 1924).
Scope: Airplane Section report prepared by A. L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.
Contents: See title.
"Aspect Ratio and Overhang for Biplane Combinations" (Bulletin of the Airplane Engineering Department, U.S.A, Vol. I, No. 3), 1918-08
Automobile Body Engineering and Surface Development: Introducing the "Replicator Method", 1946, 1946
Basic Wing and Arifoil Theory, 1951, 1951
"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.
"Comparative Evaluation of Methods for Predicting Flutter and Divergence of Unswept Wings of Finite Span" (NASA Technical Note TN D-2051), 1963-12
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2051, dated December 1963.
Scope: Preliminary NASA research report by E. Carson Yates, Jr. and Samuel R. Bland of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
