Airplanes -- Design and construction -- Research
Found in 40 Collections and/or Records:
"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.
"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.
"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.
"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.
"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.
"Effect of Tilt of the Propeller Axis on the Longitudinal-Stability Characteristics of Single-Engine Airplanes" (NACA Report No. 774), 1944
Document Type: Technical Research Report
Authority: Government Civil (authoritative reference)
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 774, published in 1944.
Scope: NACA research report by Harry J. Goett and Noel K. Delany.
Contents: See title.
"Effects of Canopy Shape on Low-Speed Aerodynamic Characteristics of a 55 degree Swept Parawing with Large-Diameter Leading Edges" (NASA Technical Note TN D-2551), 1964-12
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2551, dated December 1964.
Scope: Preliminary NASA research report by Delwin R. Croom, Rodger L. Naeseth and William C. Sleeman, Jr. of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.