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Start Over Author National Advisory Committee for Aeronautics Sudoc Stem Y 3.N 21/6

1. Technical notes. 1555. Errata. Theoretical lift of flat swept-bark wings at supersonic speeds, by Doris Cohen, Mar. 1948.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 8, 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

2. Technical notes. 1913. Method of designing airfoils with prescribed velocity distributions in compressible potential flows [with list of references]; by George R. Costello.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

3. Technical notes. 1916. Effects of sideslip, aspect ratio, and Much number on lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic How [with list of references]; by Arthur L. Jones, Robert M. Sorenson, and Elizabeth E. Lindler.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

4. Technical notes. 1919. Analytical method for determining transmission and absorption of timedependent radiation through thick absorbers: 1, Radioactivity of absorber, time dependent [with list of references]; by G. Allen.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

5. Technical notes. 1920. Preliminary investigation of needle bearings of 1⅛-inch pitch diameter at speeds to 17,000 rpm [with list of references]; by E. Fred Macks.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

6. Technical notes. 1923. Boundarv-layer and stalling characteristics of NACA 64A006 airfoil section [with list of references]; by George B. McCullough and Donald E. Gault.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

7. Technical notes. 1925. Line-vortex theory for calculation of supersonic downwash [with list of references]; by Harold Mirels and Rudolph C. Haefeli.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

8. Technical notes. 1927. Generalization of turbo jet-engine performance in terms of pumping characteristics [with list of references]; by Newell D. Sanders and Michael Behun.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

9. Technical notes. 1928. Critical combinations of shear and direct axial stress for curved rectangular panels [with list of references]; by Murry Schilderout and Manuel Stein.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

10. Technical notes. 1929. On stability of free laminar boundary layer between parallel streams [with list of references]; by Martin Lessen.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1949
SuDoc number:: Y 3.N 21/6:6/(nos.)

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