Aerodynamics
Found in 79 Collections and/or Records:
"Preliminary Wind-Tunnel Tests of the Effect of Nacelles on the Characteristics of a Twin-Engine Bomber Model with Low-Drag Wing" (NACA Advance Confidential Report, July 1942), 1942-07
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Advance Confidential Report (dated July 1942).
Scope: NACA research report by Carl J. Wenzinger and James C. Sivells.
Contents: See title.
"Report of Wind-Tunnel Test of DH-4B Model, Full Scale: 1. With 7 1/2 inch positive stagger and 2. With 2-inch positive stagger" (Air Service Information Circular (Aviation) Vol. IV, No. 355), 1921-10-07, 1922-06-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. IV, No. 355 (dated June 15, 1922), based on McCook Field Report Serial No. 1868 (dated October 7, 1921).
Scope: Report prepared by Lieut. C. L. Morse, A. S. of the Structures & Analysis Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title.
"Report of Wind-Tunnel Test on U.S.A. 27 Airfoil (Supplement to Air Service Information Circular (Aviation), Vol I, No. 49)" (Air Service Information Circular (Aviation) Vol. II, No. 198), 1920-12-08, 1921-04-25
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. II, No. 198 (dated April 25, 1921), based on McCook Field Report Serial No. 1460 (dated December 8, 1920).
Scope: Report prepared by Engineering Division, Air Service, McCook Field.
Contents: See title.
"Report of Wind Tunnel Test on U.S.A. Airfoils 30, 31, 32, 33, and 34" (Air Service Information Circular (Aviation) Vol. III, No. 244), 1921-01-28, 1921-07-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. III, No. 244 (dated July 15, 1921), based on McCook Field Report Serial No. 1539 (dated January 28, 1921).
Scope: Report prepared by Structures & Analysis Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title.
Report of Wind Tunnel Tests on Aerofoils: Dayton-Wright Nos. TT-1 and TT-2, Dayton-Wright Nos. 5 and 6, and Gottingen No. 387" (Air Service Information Circular (Aviation) Vol. IV, No. 328), 1921-10-24, 1922-03-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. IV, No. 328 (dated March 15, 1922), based on McCook Field Report Serial No. 1769 (dated October 24, 1921).
Scope: Report prepared by Structures & Analysis Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title."
"Report on Wind-Tunnel Test of Armored Pursuit Airplane PG-1, Type IV" (Air Service Information Circular (Aviation) Vol. II, No. 166), 1921-01-31, 1921-05-01
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. II, No. 166 (dated May 1, 1921 (based on McCook Field Report Serial No. 1499, dated January 31, 1921).
Scope: Report prepared by S. & A. Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title.
"Report on Wind Tunnel Test of U.S.A. 27-C Modified Airfoil" (Air Service Information Circular (Aviation) Vol. IV, No. 334), 1921-12-05, 1922-03-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. IV, No. 334 (dated March 15, 1922), based on McCook Field Report Serial No. 1789 (dated December 5, 1921).
Scope: Report prepared by Structures & Analysis Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title."
"Stabilizer and Elevator Pressure Distribution" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 3) [Photocopy], 1918-12
"Stresses in Diving and Looping" (Bulletin of the Airplane Engineering Department, U.S.A, Vol. I, No. 1), 1918-06
Sub-series I.A: Aircraft RDT&E
Includes RDT&E for commercial, military and general aviation aircraft and aircraft engines (motors). Includes basic aerodynamic and aviation materials research.