Download or read book Calculation of the Aerodynamic Loading of Flexible Wings of Arbitrary Plan Form and Stiffness written by Franklin W. Diederich and published by . This book was released on 1949 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for calculating the aerodynamic loading, the divergence speed, and certain stability derivatives of wings and tail surfaces of arbitrary plan form and stiffness. Computing forms, tables of numerical constants required in the analysis, and an illustrative example are included.

Download or read book Calculation of the Aerodynamic Loading of Flexible Wings of Arbitary Plan Form and Stiffness written by Franklin W. Diederich and published by . This book was released on 1948 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Calculation of the Aerodynamic Loading of Swept and Unswept Flexible Wings of Arbitrary Stiffness written by Franklin W. Diederich and published by . This book was released on 1950 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 1082 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Note written by and published by . This book was released on 1949 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Calculation of Aerodynamic Loading and Twist Characteristics of a Flexible Wing at Mach Numbers Approaching 1 0 and Comparison with Experiment written by John P.. Mugler and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Method for Calculating the Subsonic Steady state Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness written by W. L. Gray and published by . This book was released on 1953 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method for computing the steady-state span load distribution on an elastic airplane wing for specified airplane weights and load factors is given. The method is based on a modification of the Weissinger L-method and applies at subcritical Mach numbers. It includes the effects of external stores and fuselage on the spanwise loading. Modifications are outlined for treating tail-boom and tailless airplane configurations and for calculating the divergence dynamic pressure of a swept wing with a large external store. A method is also outlined for reducing wind-tunnel data to obtain effective aerodynamic coefficients which are free of model flexibility effects. The effects of Mach number can readily be evaluated from the aerodynamic coefficients thus obtained.

Download or read book Further Experiments on the Flow and Heat Transfer in a Heated Turbulent Air Jet written by Alfred Gessow and published by . This book was released on 1950 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Diffusion of Chromium in Alpha cobalt chromium Solid Solutions written by John W. Weeton and published by . This book was released on 1950 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt: When compared with most alloys systems for which diffusion data have been previously obtained, the diffusion rates of chromium in alpha cobalt-chromium solid solutions were found to be low.

Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Annual Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Download or read book Supersonic Aeroelastic Effects on Static Stability and Control Aeroelastic interaction by V W Donato written by Bell Aircraft Corporation and published by . This book was released on 1958 with total page 374 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Further Experiments on the Flow and Heat Transfer in a Heated Turbulent Air Jet written by Stanley Corrsin and published by . This book was released on 1949 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements have been made of the mean total-head and temperature fields in a round turbulent jet with various initial temperatures.

Download or read book Theoretical Study of the Tunnel boundary Lift Interference Due to Slotted Walls in the Presence of the Trailing vortex System of a Lifting Model written by Clarence W. Matthews and published by . This book was released on 1955 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt: