Box MC-019-002
Contains 85 Results:
"The Effect of Air Temperature Upon the Rate of Climb of an Airplane Equipped With a Constant Speed Propeller" (CAA Flight Engineering Report No. 12), 1943-12-01, 1943-11-02
"Altitude and Its Effect Upon Airplane Performance" (CAA Flight Engineering Report No. 13), 1944-06-13, 1944-07-10
"The Apparent Effect of Pilot Technique and Atmospheic Disturbances upon the Measured Rate of Climb of an Airplane" (CAA Flight Engineering Report No. 17), 1945-05-01, 1945-06-07
"The Low Drag Sailplane, Tiny Mite, Modification 1954" [Manuscript from the Aerophysics Department, Mississippi State College], 1954-08-12
Document Type: Academic Research Paper
Purpose: Scholarly reference
Authority: Author Expertise
Scope & Contents: Looks at ways to modify sailplanes to reduce drag.
"A Systematic Kernel Function Procedure for Determining Aerodynamic Forces on Oscillating or Steady Finite Wings at Subsonic Speeds" (NASA Technical Report TR R-48) [Photocopy], 1959-01-01
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Report TR R-48, dated January 1, 1959.
Scope: NASA research report by Charles E. Watkins, Donald S. Woolston and Herbert J. Cunningham of Langley Research Center, Langley Field, Va.
Contents: See title.
"Investigation of the Divergence Characteristics of Delta-Planform Canard Controls" (NASA Technical Report TR R-235) [Photocopy], 1966-04-01
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Report TR R-235, dated April 1, 1966.
Note: Supersedes "recently declassified NACA RM L58E07 by A. Gerald Rainey, Perry W. Hanson, and Dennis J. Martin, 1958.
Scope: NASA research report by A. Gerald Rainey, Perry W. Hanson and Dennis J. Martin of Langley Research Center, Langley Station, Va.
Contents: See title.
"Review of Propeller-Rotor Whirl Flutter" (NASA Technical Report TR R-264), 1967-07
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Report TR R-264, dated July, 1967.
Scope: NASA research report by Wilmer H. Reed III of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Approximation of the Spanwise Distribution of Wind-Tunnel-Boundary Interference on Lift of Wings in Rectangular Perforated-Wall Test Sections" (NASA Technical Report TR R-285), 1968-05
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Report TR R-285, dated May, 1968.
Scope: NASA research report by Ray H. Wright and Benferd L. Schilling of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Test Sections for Small Theoretical Wind-Tunnel-Boundary Interference on V / STOL Models" (NASA Technical Report TR R-286), 1968-08
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Report TR R-286, dated August, 1968.
Scope: NASA research report by Ray H. Wright of Langley Research Center, Langley Station, Hampton, Va.
Contents: See title.
"Large Scale Wind-Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft - Preliminary Results" (NASA Technical Note TN D-326) [Photocopy], 1960-10-01
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-326, dated October 1, 1960.
Scope: Preliminary NASA research report by David G. Koenig and James A. Brady.
Contents: R&D work on wingless vertical take-off and landing aircraft.