Download or read book Direct reading Design Charts for 75S T Aluminum alloy Flat Compression Panels Having Longitudinal Straight web Y section Stiffeners written by Norris F. Dow and published by . This book was released on 1948 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt: Direct-reading design charts are presented for 75S-T aluminum-alloy flat compression panels having longitudinal straight-web Y-section stiffeners. These charts make possible the direct determination of the stress and all the panel proportions required to carry a given intensity of loading with a given skin thickness and effective length of panel.

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 1949 with total page 616 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 Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Application of Green s Theorem to the Solution of Boundary value Problems in Linearized Supersonic Wing Theory written by Max A. Heaslet and published by . This book was released on 1949 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt: Under the assumptions of linearized theory, general methods of solutin are given for two- and three-dimensional steady-state and two-dimensional unsteady-state equations of compressible flow. The solutions depend in all cases on the use of Green's equivalent layer of sources, sinks, and doublets. Emphasis is placed on applications in supersonic wing theory, the singularities arising in the integrations being treated by Hadamard's finite part of the technique. Four examples of different character are discussed. In particular, the load distribution over a specific swept-back lifting surface is determined at a free-stream Mach number of one.

Download or read book Technical Note written by and published by . This book was released on 1948 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation in Climb and at High Speed Or a Two blade and Three blade Propeller written by Jerome B. Hammack and published by . This book was released on 1949 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the results obtained with a propeller in a three-blade and two-blade configuration in climb and high-speed flight when mounted on a slender-nose fighter airplane. An extensive series of power loadings were investigated up to an airplane Mach number of 0.7. The results are explained by theory. Recommendations for propeller efficiency improvement are stated.

Download or read book The Effects on Dynamic Lateral Stability and Control of Large Artificial Variations in the Rotary Stability Derivatives written by Robert O. Schade and published by . This book was released on 1952 with total page 726 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an experimental and theoretical investigation of the effects of large artificial variations of four rotary stability derivatives on the dynamic lateral stability and control of a 45 degree sweptback-wing airplane model are presented. The experimental results are presented mainly in the form of flight ratings for stability, control, and general flight behavior. Calculations of period and damping and of the response of rolling and yawing disturbances are also presented.

Download or read book A Biharmonic Relaxation Method for Calculating Thermal Stress in Cooled Irregular Cylinders written by Arthur G. Holms and published by . This book was released on 1951 with total page 700 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical method was developed for calculating thermal stresses in irregular cylinders cooled by one or more internal passages. The use of relaxation methods and elementary methods of finite differences was found to give approximations to the correct values when compared with previously known solutions for concentric circular cylinders possessing symmetrical and asymmetrical temperature distributions.

Download or read book Direct Reading Design Charts for 24S T Aluminium alloy Flat Compression Panels Having Longitudinal Straight web Y section Stiffeners written by Norris F. Dow and published by . This book was released on 1949 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1948 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1948 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.

Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft Volume 1 Structures written by Frederick O. Smetana and published by . This book was released on 1970 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book United States Government Publications Monthly Catalog written by and published by . This book was released on 1948 with total page 1606 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft Structures by Frederick O Smetana written by Frederick O. Smetana and published by . This book was released on 1970 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Contractor Report written by and published by . This book was released on 1969 with total page 972 pages. Available in PDF, EPUB and Kindle. Book excerpt: