Publish Year Decade: 1940 - 1949 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1940 - 1949 Sudoc Stem Y 3.N 21/5

1. Technical memorandum. 1196. Nonstationary gas flow in thin pipes of variable cross section, by G. Guderly; translation [by Dave Feingold].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:8/(no.)

2. Technical notes. 1742. Stability and control characteristics at low speed of airplane model having 38.7° sweptback wing with aspect ratio 4.51. taper ratio 0.54. and Conventional tall surfaces [With list of references]; by Vernard E. Lockwood and James M. Watson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

3. Technical notes. 1759. Effects of compressibility on normal-force, pressure, and load characteristics of tapered wing of NACA 66-series airfoil sections with split flaps [with list of references]; by F. E. West, jr., and J. M. Hallissy, jr.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

4. Technical notes. 1762. Control considerations for optimum power proportionment in turbinepropeller engines [with list of references]; by Marcus F. Heidmann and David Novik.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

5. Technical notes. 1762. Errata. Control considerations for optimum power proportionment in turbine-propeller engines; by Marcus F. Heidmann aad David Novik.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

6. Technical notes. 1763. Flight investigation of combined geared unbalancing-tab and servotab control system as used with all-movable horizontal tail [with list of references]; by Robert G. Mungall.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

7. Technical notes. 1764. Influence of tail length upon spin-recovery characteristics of trainer-typeairplane model [with list of references]; by Walter J. Klinar and Thomas L. Snyder.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

8. Technical notes. 1766. Wind-tunnel investigation of effects of tall length on longitudinal and lateral stability characteristics of single-propeller airplane model [with list of references]; by Harold S. Johnson.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

9. Technical notes. 1769. Flexible rectangular wing in roll at supersonic flight speeds [with list of references]; by Warren A. Tucker and Robert L. Nelson.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

10. Technical notes. 1771. Development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers [with list of references]; by Donald J. Graham.

Corporate/Agency Authors:: National Advistory Committee for Aeronautics
Publisher:: National Advistory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

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