Journal of the Franklin Institute, Volume 252Pergamon Press, 1951 Vols. 1-69 include more or less complete patent reports of the U. S. Patent Office for years 1825-1859. cf. Index to v. 1-120 of the Journal, p. [415] |
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Results 1-3 of 27
Page 182
... Wing , Center Section . Size 36 ′′ × 16 ′′ . Brown wrapping paper . 1.15 - Right and Left Wing Tip Panels . Cloth cover details . Size 33 " × 12 " . Brown wrapping paper . 1.16 - Fitting Details . Rudder , center section and rear strut ...
... Wing , Center Section . Size 36 ′′ × 16 ′′ . Brown wrapping paper . 1.15 - Right and Left Wing Tip Panels . Cloth cover details . Size 33 " × 12 " . Brown wrapping paper . 1.16 - Fitting Details . Rudder , center section and rear strut ...
Page 183
... Wing , Center Section . Size 36 " X 16 " . Brown wrapping paper . 1.15 - Right and Left Wing Tip Panels . Brown wrapping paper . Cloth cover details . Size 33 " X 12 " . 1.16 - Fitting Details . Rudder , center section and rear strut ...
... Wing , Center Section . Size 36 " X 16 " . Brown wrapping paper . 1.15 - Right and Left Wing Tip Panels . Brown wrapping paper . Cloth cover details . Size 33 " X 12 " . 1.16 - Fitting Details . Rudder , center section and rear strut ...
Page 189
... Wing . Clark ( USA 27C ) Tapered wing - L / D vs. lift . Size 11 " x 17 " -T 1 May 19 , 1922 , Clark Dec. 13 , 1920 . 13.31 Graph . Bauman Gordon Bennett Racer . L / D vs. Lift . Size 11 " X 17 " . Dated Mar. 9 , 1921 . 13.32 Graph ...
... Wing . Clark ( USA 27C ) Tapered wing - L / D vs. lift . Size 11 " x 17 " -T 1 May 19 , 1922 , Clark Dec. 13 , 1920 . 13.31 Graph . Bauman Gordon Bennett Racer . L / D vs. Lift . Size 11 " X 17 " . Dated Mar. 9 , 1921 . 13.32 Graph ...
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airfoils Angle of Attack application Area 6 sq atomic BIPLANE bottom boundary value problems Brown wrapping paper Bureau Camber cent chapters charge Chord Company concrete contact potential coordinate cos² cosh curve cylinder Dayton Wright developed distribution electric electrons engineering equipment field film foot valve Franklin Institute function Graph Helmholtz equation humidity hydraulic hydrazine industry interflectance inversion ionosphere Laboratories Laplace transform Laplace's equation Lift light luminaires magnetic material mathematical measurements mechanism Metal Model method multiple transform obtained operation Orville Wright partial differential equation pharosage plate problems produced pulse Section sin² sinh slow discharge Span 18 Superposed surface Table temperature Test block theory tion tremie pipe tube valve variables waveforms Wax Model Wax on Metal Wind Tunnel Wind Tunnel Test Wing wire μ²