Aircraft Engine Historical Society, Inc.
Found in 437 Collections and/or Records:
"Aerodynamic Data On a Large Semispan Tilting Wing with 0.6-Diameter Chord, Fowler Flap, and Single Propeller Rotating Up At Tip" (NASA Technical Note TN D-2180), 1964-02
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2180, dated February 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 Data on Large Semispan Tilting Wing with 0.6-Diameter Chord, Single-Slotted Flap, and Single Propeller Rotating Down at Tip" (NASA Technical Note TN D-2412), 1964-08
Document Type: Technical Research Report.
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NASA Technical Note TN D-2412, dated August 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 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.
"Aerodynamics Of The Fuselage" [Translation of paper titled "Zur Aerodynamik des Flugzeugrumpfenes" by H. Multhopp]" (NACA Technical Memorandum No. 1036), 1941-03-29, 1942-12
Document Type: Technical Research Report (Translation).
Purpose: Authoritative reference
Authority: Government Civil
Document Number: NACA Technical Memorandum No.1036, dated December 1942. Originally published in German in Luftfahrtforschung, Vol. 18, No. 2-3, March 29, 1941, pages 52-56.
Scope: Translation of academic paper titled "Zur Aerodynamik des Flugzeugrumpfenes" by H. Multhopp.
Contents: See title.
"Aileron Effectiveness: Wind Tunnel Tests of U.S.A.-35 (Half-Span) Airfoil with Skewed Ailerons" (Air Service Information Circular (Aviation) Vol. V, No. 454), 1923-11-05, 1924-03-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. V, No. 454 (dated March 15, 1924), based on McCook Field Report Serial No. 2252 (dated November 5, 1923).
Scope: Airplane Section report prepared by A.L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.
Contents: See title.
"Aileron Effectiveness: Wind Tunnel Tests of U.S.A.-35 (Half-Span) Airfoil with Skewed Ailerons" (Air Service Information Circular (Aviation) Vol. V, No. 454), 1923-11-05, 1924-03-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. V, No. 454 (dated March 15, 1924), based on McCook Field Report Serial No. 2252 (dated November 5, 1923).
Scope: Airplane Section report prepared by A.L. Morse, Engineering Division, Air Service, McCook Field, Dayton, Ohio.
Contents: See title.