132,95 €
132,95 €
inkl. MwSt.
Sofort per Download lieferbar
payback
66 °P sammeln
132,95 €
132,95 €
inkl. MwSt.
Sofort per Download lieferbar

Alle Infos zum eBook verschenken
payback
66 °P sammeln
Als Download kaufen
132,95 €
inkl. MwSt.
Sofort per Download lieferbar
payback
66 °P sammeln
Jetzt verschenken
132,95 €
inkl. MwSt.
Sofort per Download lieferbar

Alle Infos zum eBook verschenken
payback
66 °P sammeln
  • Format: ePub

Aerodynamic Heating in Supersonic and Hypersonic Flows: Advanced Techniques for Drag and Aero-heating Reduction explores the pros and cons of different heat reduction techniques on other characteristics of hypersonic vehicles. The book begins with an introduction of flow feature around the forebody of space vehicles and explains the main parameters on drag force and heat production in this region. The text then discusses the impact of severe heat production on the nose of hypervelocity vehicles, different reduction techniques for aerodynamic heating, and current practical applications for…mehr

  • Geräte: eReader
  • mit Kopierschutz
  • eBook Hilfe
  • Größe: 121.86MB
Produktbeschreibung
Aerodynamic Heating in Supersonic and Hypersonic Flows: Advanced Techniques for Drag and Aero-heating Reduction explores the pros and cons of different heat reduction techniques on other characteristics of hypersonic vehicles. The book begins with an introduction of flow feature around the forebody of space vehicles and explains the main parameters on drag force and heat production in this region. The text then discusses the impact of severe heat production on the nose of hypervelocity vehicles, different reduction techniques for aerodynamic heating, and current practical applications for forebody shock control devices. Delivers valuable insight for aerospace engineers, postgraduate students, and researchers.
  • Presents computational results of different cooling systems for drag and heat reduction around nose cones
  • Explains mechanisms of drag reduction via mechanical, fluidic, and thermal systems
  • Provides comprehensive details about the aerodynamics of space vehicles and the different shock features in the forebody of super/hypersonic vehicles
  • Describes how numerical simulations are used for the development of the current design of forebody of super/hypersonic vehicles

Dieser Download kann aus rechtlichen Gründen nur mit Rechnungsadresse in A, B, BG, CY, CZ, D, DK, EW, E, FIN, F, GR, HR, H, IRL, I, LT, L, LR, M, NL, PL, P, R, S, SLO, SK ausgeliefert werden.

Autorenporträt
Dr. Mostafa Barzegar Gerdroodbary is a Research Associate at Babol Noshirvani University of Technology. He obtained his Ph.D. in Mechanical Engineering at Babol Noshirvani University of Technology, IRAN in 2019. He completed his Ph.D. on modelling of rarefied gas flow for calibration of gas sensor using DSMC. He published two authored books (Scramjets: fuel mixing and injection systems, Aerodynamic Heating in Supersonic and Hypersonic Flows) and two book chapters (Gas Sensors, Nanotechnology for Light Pollution Reduction) and more than 70 journal articles in high rank journals. For his outstanding research, Dr. Barzegar was included in the World's Top 2% Scientists 2021 list (by Stanford University). He is also a member of the editorial board for many journals such as Scientific Report.