Aerodynamic Heating in Supersonic and Hypersonic Flows: Advanced Techniques for Drag and Aero-heating Reduction
Autor Mostafa Barzegar Gerdroodbaryen Limba Engleză Paperback – 12 oct 2022
- 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
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Specificații
ISBN-13: 9780323917704
ISBN-10: 0323917704
Pagini: 246
Dimensiuni: 152 x 229 x 22 mm
Greutate: 0.34 kg
Editura: ELSEVIER SCIENCE
ISBN-10: 0323917704
Pagini: 246
Dimensiuni: 152 x 229 x 22 mm
Greutate: 0.34 kg
Editura: ELSEVIER SCIENCE
Public țintă
Postgrad aerospace engineering students; engineers, researchers and those involved in the design of shuttles and hypersonic vehicles.Cuprins
1. Introduction
2. Mechanical techniques (spike)
3. Fluidic techniques, opposing (counterflow) jets
4. Energetic (thermal) devices, energy deposition devices
5. Hybrid technique
6. Current practical applications for forebody shock control devices
2. Mechanical techniques (spike)
3. Fluidic techniques, opposing (counterflow) jets
4. Energetic (thermal) devices, energy deposition devices
5. Hybrid technique
6. Current practical applications for forebody shock control devices