Author: National Advisory Committee for Aeronautics / Publish Year Decade: 1940 - 1949 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Publish Year Decade 1940 - 1949

701. Boundary layer. Wind-tunnel investigation of boundary layer and wake and their relation to airfoil characteristics, NACA 651-012 airfoil with true contour flap and beveled-trailing-edge flap [with list of references]; by Robert A. Mendelsohn.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1304

702. Columns. Local buckling strength of lipped Z-columns with small lip width [with list of references]; by Pai C. Hu and James C. McCulloch.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1335

703. Cylinders. Critical combinations of torsion and direct axial stress for thin-walled cylinders [with list of references]; by S. B. Batdorf, Manuel Stein, and Marry Schildcrout.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1345

704. Cylinders. Critical stress of thin-walled cylinders in axial compression [with list of references]: by S. B. Batdorf, Murry Schildcrout, and Manuel Stein.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1343

705. Cylinders. Critical stress of thin-walled cylinders in torsion [with list of references]; by S. B. Batdorf, Manuel Stein, and Murry Schilderout.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1344

706. Cylindrical shells. Simplified method of elastic-stability analysis for thin cylindrical shells: 1, Donnell's equation [with list of references]; by S. B. Batdorf.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1341

707. Cylindrical shells. Simplified method of elastic-stability analysis for thin cylindrical shells: 2. Modified equilibrium equation [with list of references]; by S. B. Batdorf.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1342

708. Engines. Description of Russian aircraft engines AM35 and AM38. by H. Denkmeier and K. Gross; [translation by Edward S. Shafer].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:8/1169

709. Fans. Effect, of critical Mach number and flutter on maximum power loading of ducted fans [with list of references]: by Arthur A. Regier, John G. Barmby, and Harvey H. Hubbard.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:6/1330

710. Flaps (aircraft). Lift increase by blowing out air, tests on airfoil of 12 percent thickness, using various types of flap [with list of references], by W. Schwier; translation [by H. Pikler].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1947
SuDoc number:: Y 3.N 21/5:8/1148

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