Rate-dependent energetic processes in hypersonic flows

Author:

Candler Graham V.

Funder

Air Force Office of Scientific Research

Department of Defense National Security Science & Engineering Faculty Fellowship

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference26 articles.

1. Basic governing equations for the flight regimes of aeroassisted orbital transfer vehicles;Lee,1985

2. Gnoffo PA, Gupta RN, Shinn JL. Conservation equations and physical models for hypersonic air flows in thermal and chemical nonequilibrium. NASA TP-2867; 1989.

3. The computation of hypersonic ionized flows in chemical and thermal nonequilibrium;Candler;J Thermophys Heat Transf,1991

4. Candler GV, Subbareddy PK, Brock JM. Advances in CFD methods for hypersonic flows, J Spacecr Rockets, 10.2514/1.A33023, forthcoming.

5. Candler GV, Subbareddy PK, Nompelis I. CFD Methods for hypersonic flows and aerothermodynamics, Prog Aeronaut Astronaut, forthcoming.

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