Download or read book A Simple Estimate of the Profile Drag of Swept Wings Addendum written by D. A. Kirby and published by . This book was released on 1952 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Simple Estimate of the Profile Drag of Swept Wings written by J. Weber and published by . This book was released on 1952 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 1460 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Download or read book Charts for the Calculation of the Wave Drag of Swept Wings written by H. Multhopp and published by . This book was released on 1950 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Synthesis of Subsonic Airplane Design written by E. Torenbeek and published by Springer Science & Business Media. This book was released on 2013-06-29 with total page 607 pages. Available in PDF, EPUB and Kindle. Book excerpt: Since the education of aeronautical engineers at Delft University of Technology started in 1940 under tae inspiring leadership of Professor H.J. van der Maas, much emphasis has been placed on the design of aircraft as part of the student's curriculum. Not only is aircraft design an optional subject for thesis work, but every aeronautical student has to carry out a preliminary airplane design in the course of his study. The main purpose of this preliminary design work is to enable the student to synthesize the knowledge ob tained separately in courses on aerodynamics, aircraft performances, stability and con trol, aircraft structures, etc. The student's exercises in preliminary design have been directed through the years by a number of staff members of the Department of Aerospace Engineering in Delft. The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years. Not only has he acquired vast experience in teaching airplane design at university level, but he has also been deeply involved in design-oriented re search, e.g. developing rational design methods and systematizing design information. I am very pleased that this wealth of experience, methods and data is now presented in this book.

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Estimation of Swept Wing Drag at Supersonic Speeds written by T. Lawrence and published by . This book was released on 1953 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Methods for Estimating Drag Polars of Subsonic Airplanes written by Jan Roskam and published by . This book was released on 1971 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index Aeronauticus written by and published by . This book was released on 1964-07 with total page 572 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Current Papers written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1974 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Note on the Drag Due to Lift of Rectangular Wings of Low Aspect written by Edward C. Polhamus and published by . This book was released on 1955 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Methods of estimating the induced drag of low-aspect-ratio wings are discussed and compared with experiment. The profile drag due to lift is also discussed and a method is developed which relates the effect of aspect ratio on the profile drag due to lift to an "effective" two-dimensional lift coefficient. A simple expression for this effective two-dimensional lift coefficient in terms of the aspect ratio is derived and used to correlate experimental values of profile drag due to lift for rectangular wings in the low-aspect-ratio range. A method of utilizing two-dimensional test results, by means of this effective two-dimensional lift coefficient, to estimate the profile drag due to lift of low-aspect-ratio wings is briefly discussed.

Download or read book Papers Presented at the Seventh Meeting of the Wind Tunnel and Model Testing Panel written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development and published by . This book was released on 1955 with total page 1010 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1972 with total page 790 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.

Download or read book Papers written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development and published by . This book was released on 1955 with total page 358 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Papers Presented at the Seventh Meeting of the Wind Tunnel and Model Testing Panel written by North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Wind Tunnel and Model Testing Panel. Meeting and published by . This book was released on 1955 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Boundary Layer Effects in Aerodynamics written by National Physical Laboratory (Great Britain) and published by . This book was released on 1955 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt: