Airplanes -- Fuselage
Found in 11 Collections and/or Records:
"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.
"Force- and Pressure-Distrubution Measurements on Eight Fuselages" [Translation of paper titled "Kraftmessungen und Druckverteilungsmessungen an 8 Rümpfen" by G. Lange] (NACA Technical Memorandum No. 1194), 1941-10-24, 1948-10
"Recommendations for Numerical Solution of Reinforced-Panel and Fuselage-Ring Problems (NACA Report No. 934), 1949
Document Type: Technical Research Report.
Authority: Government Civil (authoritative reference).
Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 934, published in 1949.
Scope: NACA research report by N. J. Hoff and Paul A. Libby of the Polytechnic Institute of Brooklyn (under a NACA contract).
Contents: See title.
"Report of Static Test of GAX-1 Chassis" (Air Service Information Circular (Aviation) Vol. II, No. 171), 1920-11-03, 1920-12-27
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. II, No. 171 (dated December 27, 1920 (based on McCook Field Report Serial No. 1406, dated November 3, 1920).
Scope: Report prepared by S. & A. Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title.
"Report of Static Test of XB-1-A Fuselage" (Air Service Information Circular (Aviation) Vol. IV, No. 338), 1922-01-04, 1922-05-01
"Scientific Fairing of Veneer Fuselages" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 1), 1918-10
"Structural Design of Cabane Struts for the PW-1 with R.A.F. 15 Tapered Wings" (Air Service Information Circular (Aviation) Vol. II, No. 172), 1920-09-21, 1921-01-15
Document Type: Technical Research Report
Authority: Government Military (authoritative reference)
Document Number: Air Service Information Circular (Aviation) Vol. II, No. 172 (dated January 13, 1921 (based on McCook Field Report Serial No. 1376, dated September 21, 1920).
Scope: Report prepared by S. & A. Branch, Airplane Section, Engineering Division, Air Service, McCook Field.
Contents: See title.