electronic library
metadata only
NUMERICAL INVESTIGATION OF THE THERMAL BENEFIT OF USING A HIGH THERMAL CONDUCTIVITY CMC FOR THE LEADING EDGE OF HYPERSONIC VEHICLES
During atmospheric re-entry high thermal loads are generated on the surface of the entry vehicle with peak loads in the stagnation area. Typical entry vehicles have a blunt shape avoiding sharp tips or leading edges. Recent developments for vehicles in the hypersonic flight regime have concentrated
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- Heat pipes with variable thermal conductance property developed for space applications#246308
- Residual stresses in Cu matrix composite surface deposits after laser melt injection#226935
- Does the Boussinesq approximation correctly describe statistically stationary states of Rayleigh-Bénard convection?#1160741
- Heat Therapy and Cardiometabolic Health in Obese Women#836416
- Broadband low-frequency sound absorption and high insulation in a clay-cement composite with hydrogel-foaming engineered gradient porosity.#159884
Record · ID 1089794
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive