Idioma: Inglés
Publicado por Center for Incentive Taxation; Shepheard-Walwyn: London; Holmes & Meier: NY, 1991
ISBN 10: 0856831247 ISBN 13: 9780856831249
Librería: Berry Hill Book Shop, Deansboro, NY, Estados Unidos de America
EUR 11,26
Cantidad disponible: 1 disponibles
Añadir al carritoHardcover. Condición: Near Fine. 1991, About Fine/Near Fine dj, octavo, 241pp., blue boards hardcover, bright gold lettering on backstrip, excellent pictorial unclipped dj, binding tight, text unmarked.
Publicado por Clark Publishing Co., Evanston, IL, 1954
Librería: biblioboy, North Providence, RI, Estados Unidos de America
Original o primera edición
EUR 13,51
Cantidad disponible: 1 disponibles
Añadir al carritoSingle Issue Magazine. Condición: Good. First Edition. Clark Publishing 1954 1st ed. 130pp Good condition with wear and creasing to covers, tear and chip to spine about an inch down from head. Previous owner stamps to front cover, toning to pages. bx811E.
Publicado por London: To-Day, 1921
Librería: Benedict Wilson Books, Folkestone, KENT, Reino Unido
Original o primera edición
EUR 24,22
Cantidad disponible: 1 disponibles
Añadir al carritoSoft cover. Condición: Very Good. 1st Edition. FIRST EDITION. Octavo (20 x 15cm), pp.x; 133-172; xi-xiv. Publisher's card wraps printed in red and black, price of one shilling net to upper. Some spotting to edges and covers, staples rusted, lightly handled. Very good.
Publicado por Selbstverlag, 1947
Librería: Versandantiquariat Funke, Dresden, Alemania
EUR 85,00
Cantidad disponible: 1 disponibles
Añadir al carritoCondición: sehr guter Zustand. F. sehr guter Zustand, geringe Gebrauchs- und Alterungsspuren: Deckel und erste Textseite mit altem Stempel, Deckel auch noch mit Nummer - Umschlag und Seiten teils etwas eselsohrig - Seiten sauber und ordentlich Presents analysis of composite engine comprising piston engine, blowdown turbine, and steady-flow turbine with particular emphasis on cost of design compromises in operation of the engine over the range of altitudes and powers. For geared-in turbines, compressor losses were sometimes large and the altitude range was restricted. By the use of an auxiliary propeller, these losses could be reduced. The weights of the engines were not considered in the evaluation. Buchreihe: Technical Note, NACA 1447 Seitenanzahl: 56 Seiten mit 14 Bildern und 6 Karteikarten Format: ca. 19,5 x 26 kartoniert Englisch.