Get Aircraft of the Second World War: The Development of the PDF

By Phillip Jarrett

ISBN-10: 0851778755

ISBN-13: 9780851778754

Airplane of the second one international battle: the improvement of the Warplane 1939-45 ВОЕННАЯ ИСТОРИЯ,ТЕХНИКА Название: plane of the second one global conflict: the advance of the Warplane 1939-45Автор: Philip JarrettИздательство: Putnam Aeronautical BooksISBN: 0851778755Год: 1997Страниц: 304Формат: PDF в RARРазмер: 168.8МБКачество: хорошееЯзык: английскийThis is a examine of plane from international conflict II. The publication is a part of a 12volume sequence, which covers the construction and operation of plane world wide. each one quantity is dedicated to essays on plane varieties, their improvement and alternative, platforms and equipment.As good as outlining advancements, each one article seeks to provide an explanation for why growth was once in a selected path, emphasizing the political, strategic or fiscal components that dictated that improvement. relocating from the overall to the categorical, graphs and tabular info with regards to standard or major plane or allied matters are supplied in each one section.The sequence concentrates at the improvement of plane from the point of view in their technical improvement, the impact of technical improvement at the use of airplane, and the impression in their utilization on technical improvement. Скачать:LetitbitDepositfiles zero

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Extra info for Aircraft of the Second World War: The Development of the Warplane 1939-45

Example text

Mit zunehmender Schlankheit, zu hOheren Machschen Zahlen verschiebt. h. 088 q064 frofildiCkenverhtiltfiS e-t/d q056 I q048 Ca-o II I1 6-12% I I fX=O° q032 0-6% q024 qOl6 HkNf/ P q008 o 6-1/5% '1,6-9% q040 e.. I CwSlim-0,4 belogen \ auf die stirnflacl1e r----. q072 Abb. 23. Profilwiderstandsbeiwert cWI> in Abhangigkeit der Machschen Zahl M, fiir einige symmetrische NACAProfile mit verschiedenem Profildickenverhaltnis. Mkrit = kritische Machsche Zahl. N ach F. FELDMANN, Interavia, 1946, S. 60, Genf.

Diese Ablenkung erfolgt gegen den Storkorper hin, was man Ieicht seIber nachprufen kann, indem man einen Finger, zum Beispiel den Daumen, an einen Wasserstrahl halt. Einfluss der Profilform auf die kritische Machsche Zahl 57 Zufuhrung der heiBen Triebwerkgase zu der Flugelhinterkante und Li:isung der damit verbundenen technologischen Probleme; Unterbringung des Kraftstoffes im Flugel; Verhindern des Platzens der uber dem Flugel liegenden Unterdruckblase bei positiver Anstellung des Flugels, zur Verhutung eines Auftriebszusammenbruches.

Folgender Umstand muB besonders herausgestrichen werden: Sobald sich an der engsten Stelle der Diise Schallgeschwindigkeit einstellt, verursacht auch jede weitere Absenkung des Gegendruckes keine VergroBerung der Geschwindigkeit an Po a der engsten Stelle, da sich Druck9 b anderungen nur mit Schallgeschwindigkeit ausbreiten konnen. Irgendwelche Einwirkungen von - f stromabwarts gelegenen Stellen i p stromaufwarts sind daher nicht moglich. Damit bleibt auch die ~------~~~------~=e x ---___ DurchfluBmenge vom Gegendruck unabhangig.

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Aircraft of the Second World War: The Development of the Warplane 1939-45 by Phillip Jarrett


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