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Author: Alexander Lippisch
Publisher: Iowa State Press
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 144
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Book Description
Den tyske flykonstruktør beskriver her udviklingen og forsøgene med Tailless- og Delta Wing- flytyper.
Author: Alexander Lippisch
Publisher: Iowa State Press
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 144
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Book Description
Den tyske flykonstruktør beskriver her udviklingen og forsøgene med Tailless- og Delta Wing- flytyper.
Author: David E. Fetterman
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 72
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Book Description
Author: Alexander Lippisch
Publisher:
ISBN: 9780608132624
Category :
Languages : en
Pages : 136
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Book Description
Author: Andreas Dillmann
Publisher: Springer Nature
ISBN: 3030252531
Category : Technology & Engineering
Languages : en
Pages : 862
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Book Description
This book gathers contributions to the 21st biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. The book’s primary emphasis is on aerodynamic research in aeronautics and astronautics, and in ground transportation and energy as well.
Author: Bill Rose
Publisher: Secret Projects
ISBN: 9781857803204
Category : Airplanes, Tailless
Languages : en
Pages : 0
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Book Description
This is an exciting new addition to the highly successful Secret Projects series, which examines some extraordinary flying wings and tailless aircraft projects. Designed and developed since the dawn of aviation, these aircraft still hold a great importance today, with many aviation enthusiasts eager to learn more about these remarkable aircraft, which provided the foundations for the modern aviation scene. Beginning with an analysis of the advantages of the flying wing, the author looks at why aerodynamicists have been attracted to this unique configuration since the earliest days of manned flight, highlighting a range of specific aircraft and relevant examples. Many aviation enthusiasts will delight in discovering the more intimate developmental details of familiar aircraft including the famous early glider Junkers and other World War 1 flying wing biplane designs.
Author: Ernst Heinrich Hirschel
Publisher: Springer Nature
ISBN: 366261328X
Category : Technology & Engineering
Languages : en
Pages : 458
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Book Description
Fluid mechanical aspects of separated and vortical flow in aircraft wing aerodynamics are treated. The focus is on two wing classes: (1) large aspect-ratio wings and (2) small aspect-ratio delta-type wings. Aerodynamic design issues in general are not dealt with. Discrete numerical simulation methods play a progressively larger role in aircraft design and development. Accordingly, in the introduction to the book the different mathematical models are considered, which underlie the aerodynamic computation methods (panel methods, RANS and scale-resolving methods). Special methods are the Euler methods, which as rather inexpensive methods embrace compressibility effects and also permit to describe lifting-wing flow. The concept of the kinematically active and inactive vorticity content of shear layers gives insight into many flow phenomena, but also, with the second break of symmetry---the first one is due to the Kutta condition---an explanation of lifting-wing flow fields. The prerequisite is an extended definition of separation: “flow-off separation” at sharp trailing edges of class (1) wings and at sharp leading edges of class (2) wings. The vorticity-content concept, with a compatibility condition for flow-off separation at sharp edges, permits to understand the properties of the evolving trailing vortex layer and the resulting pair of trailing vortices of class (1) wings. The concept also shows that Euler methods at sharp delta or strake leading edges of class (2) wings can give reliable results. Three main topics are treated: 1) Basic Principles are considered first: boundary-layer flow, vortex theory, the vorticity content of shear layers, Euler solutions for lifting wings, the Kutta condition in reality and the topology of skin-friction and velocity fields. 2) Unit Problems treat isolated flow phenomena of the two wing classes. Capabilities of panel and Euler methods are investigated. One Unit Problem is the flow past the wing of the NASA Common Research Model. Other Unit Problems concern the lee-side vortex system appearing at the Vortex-Flow Experiment 1 and 2 sharp- and blunt-edged delta configurations, at a delta wing with partly round leading edges, and also at the Blunt Delta Wing at hypersonic speed. 3) Selected Flow Problems of the two wing classes. In short sections practical design problems are discussed. The treatment of flow past fuselages, although desirable, was not possible in the frame of this book.
Author: Captain Eric Brown CBE DSC AFC QCVSA RN
Publisher: The History Press
ISBN: 0752476912
Category : Transportation
Languages : en
Pages : 176
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Book Description
In December 1943, a top secret contract (E.24/43) was awarded to Miles Aircraft. The contract was to build the world's first supersonic jet capable of 1000mph. The only reliable source of data on supersonic objects came from the Armament Research Dept and their wind tunnel tests on ammunition. From this, Miles developed an exceptionally thin-winged, bullet-shaped aircraft. the research was inexplicably passed to the Americans in 1944. By December 1945, one prototype was virtually complete. The second, destined for an attempt at the sound barrier was 80 per cent complete. In February 1946, Capt Eric Brown was confirmed as the test pilot and October 1946 was set for the supersonic trials. However, on 12 February 1946, Miles were ordered to stop production. No plausible explanation was given for the cancellation when Britain was within six months of breaking the sound barrier. Eric Brown and others directly involved including Dennis Bancroft, the Chief Aerodynamicist on the M.52, have now come together to try and finally solve the mystery behind the cancellation.
Author: Eudora Welty
Publisher: HMH
ISBN: 0547538685
Category : Fiction
Languages : en
Pages : 339
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Book Description
This novel of a Mississippi family in the 1920s “presents the essence of the Deep South and does it with infinite finesse” (The Christian Science Monitor). From one of the most treasured American writers, winner of a National Book Award and Pulitzer Prize, comes Delta Wedding, a vivid and charming portrait of Southern life. Set in 1923, the story is centered on the Fairchilds, a big and clamorous family, who live on a plantation in the Mississippi delta. They are in the midst of planning their daughter’s wedding when a nine-year-old relative, Laura McRaven, whose mother has just died, comes to visit. Drama leads to drama, revelation to revelation, in a novel that is “nothing short of wonderful” (The New Yorker). The result is a sometimes-riotous view of a Southern family, and the parentless child who learns to become one of them.
Author: Mark Frankel
Publisher: Specialty PressPub & Wholesalers
ISBN: 9781580071550
Category : History
Languages : en
Pages : 239
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Book Description
The author unlocks secrets of delta-wing design and covers the intense rivalry between the Navy's F4D and Air Force F-102 in the 1950s.
Author: Daniel P. Raymer
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563478291
Category : Airplanes
Languages : en
Pages : 0
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Book Description
Winner of the Summerfield Book Award Winner of the Aviation-Space Writers Association Award of Excellence. --Over 30,000 copies sold, consistently the top-selling AIAA textbook title This highly regarded textbook presents the entire process of aircraft conceptual designfrom requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studiesin the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 800 pages of design methods, illustrations, tips, explanations, and equations, and extensive appendices with key data essential to design. It is the required design text at numerous universities around the world, and is a favorite of practicing design engineers.
