Author: Library of Congress / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author Library of Congress Sudoc Stem Y 3.N 21/5

1. Automatic stabilization [with list of references], by Fr. Haus: [translation by S. Reiss from] PAeronautique, Oct. 1935, Jan. and Feb. 1936.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1936
SuDoc number:: Y 3.N 21/5:8/802

2. Engines. Friction of compression-ignition engines [with list of references]; by Charles S. Moore and John H. Collins, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1936
SuDoc number:: Y 3.N 21/5:6/577

3. Hulls (aircraft). Tank tests of model of hull of Navy PB-1 flying boat, N. A. C. A. model 52 [with list of references]; by John M. Allison.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1936
SuDoc number:: Y 3.N 21/5:6/576

4. Hulls (aircraft). Tank tests of models of flying boat hulls having longitudinal steps [with list of references]; by John M. Allison and Kenneth E. Ward.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1936
SuDoc number:: Y 3.N 21/5:6/574

5. Airfoils. Contribution to problem of airfoils spanning free jet [with list of references], by J. Stüper; [translation by S. Reiss from] Luftfahrtforschung, v. 12, no. 8, Dec. 25, 1935.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1936
SuDoc number:: Y 3.N 21/5:8/796

6. Flaps (aircraft). Method of estimating aerodynamic effects of ordinary and split flaps of airfoils similar to Clark Y [with list of references]; by H. A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1936
SuDoc number:: Y 3.N 21/5:6/571

7. Spin (aircraft). Effect of changes in tail arrangement upon spinning of low-wing monoplane model [with list of references]; by C. H. Zimmerman.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1936
SuDoc number:: Y 3.N 21/5:6/570

8. Engines. Boosted performance of compression-ignition engine with displacer piston [with list of references]; by Charles S. Moore and Hampton H. Foster.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1936
SuDoc number:: Y 3.N 21/5:6/569

9. Hydrodynamics. Similitude in hydrodynamic tests involving planing [with list of references], by M. F. Gruson; [translation by Starr Truseott], presented on occasion of inauguration of Institute of Mechanics of Fluids of University of Lille, Apr. 5-8, 1984.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1936
SuDoc number:: Y 3.N 21/5:8/795

10. Airplanes. Simplified application of method of operators to calculation of disturbed motions of airplane, [with list of references]; by Robert T. Jones.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics and Library of Congress
Publisher:: National Advisory Committee for Aeronautics
Date:: 1936
SuDoc number:: Y 3.N 21/5:5/560

« Previous
Next »
1 Current Page, Page 1
2