Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56 (PDF)

Name: Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56
Brand: Springer-Verlag GmbH
SKU: 131245532
Price: 223.63 EUR
Availability: OnlineOnly

(Sprache: Englisch)

Autor: Kunyuan Zhang

Schreiben Sie einen Kommentar zu "Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56".

Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56, Kunyuan Zhang

Merken

Mehr zum Inhalt Autorenporträt Video

eBook (pdf) 223.63 €

Buch (Gebunden) 235.39 €

sofort als Download lieferbar

Bestellnummer: 131245532

Printausgabe 235.39 €

eBook (pdf) -5% 223.63 €

Download bestellen

Verschenken

111 DeutschlandCard Punkte sammeln

Lastschrift, Kreditkarte, Paypal, Rechnung
Kostenloser tolino webreader

Produktdetails

Produktbeschreibung
Autorenporträt
eBook Hilfe
Biblio. Angaben / Produktdetails

Produktinformationen zu „Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56 (PDF)“

This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic-hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author's research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.

Autoren-Porträt von Kunyuan Zhang

Prof. Kunyuan Zhang is a Professor at the College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, China. He received his B.S. and M.S. degrees in Power Engineering from Nanjing Aeronautical Institute (now Nanjing University of Aeronautics and Astronautics) in 1965 and 1981, respectively, and he has been teaching at the same university since 1986. His research fields include hypersonic propulsion technology and internal flow dynamics.

eBook Hilfe

Informationen und Hilfe zu eBooks hier klicken!

Bibliographische Angaben

Autor: Kunyuan Zhang
2020, 1st ed. 2020, 332 Seiten, Englisch
Verlag: Springer-Verlag GmbH
ISBN-10: 9811507279
ISBN-13: 9789811507274
Erscheinungsdatum: 22.01.2020

Abhängig von Bildschirmgröße und eingestellter Schriftgröße kann die Seitenzahl auf Ihrem Lesegerät variieren.

eBook Informationen

Dateiformat: PDF
Größe: 21 MB
Ohne Kopierschutz
Vorlesefunktion

Sprache:

Englisch

Kommentar zu "Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56"

Schreiben Sie einen Kommentar zu "Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56".

Wie funktionieren Bewertungen?

0 Gebrauchte Artikel zu „Hypersonic Curved Compression Inlet and Its Inverse Design / Advanced Topics in Science and Technology in China Bd.56“

Zustand	Preis	Porto	Zahlung	Verkäufer	Rating