A New Methodology to Preliminary Design Structural Components of Re-Entry and Hypersonic Vehicles

doi 10.5772/17141
Full Text
Abstract

Available in full text

Date
Authors
Publisher

InTech

Related search

Propulsion Integration of Hypersonic Air-Breathing Vehicles Utilizing a Top-Down Design Methodology

English

Computational Aerothermodynamic Design Issues for Hypersonic Vehicles

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
1999English

Design of a Re-Entry Experiment to Measure Aeroshell Heating Rates

English

The Altitude of Stabilization for Slowly Tumbling Re-Entry Vehicles

1961English

Three-Dimensional Computational Model of Nonequilibrium Aerophysics of Mars Re-Entry Vehicles

Computational Continuum Mechanics
2010English

A Method to Compute Flameout Limits of Scramjet-Powered Hypersonic Vehicles

2015English

Adjoint-Based Aerothermodynamic Shape Design of Hypersonic Vehicles in Non-Equilibrium Flows

2014English

A Multi-Criteria Decision Aid Methodology to Design Electric Vehicles Public Charging Networks

AIP Advances
NanotechnologyAstronomyPhysicsNanoscience
2015English

Re-Entry Trajectory Design Using Pigeon Inspired Optimization

2017English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy