Fundamental Relationships for Ablation and Hyperthermal Heat Transfer
Report Number: AFFDL TR 66-25
Author(s): Achard, Robert T.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Pages: 54
Contract: Laboratory Research - No Contract
DoD Project: 1368
DoD Task: 136804
Identifier: AD0633677
Abstract:
A qualitative review of fundamental relationships involved in ablation engineering and aerodynamic heating is presented. This document is written for rapid reading with the primary purpose of introducing the technical area to engineers, scientists, and management personnel associated with but not intimately working in hypervelocity thermal protection.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Achard, Robert T.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-04
Pages: 54
Contract: Laboratory Research - No Contract
DoD Project: 1368
DoD Task: 136804
Identifier: AD0633677
Abstract:
A qualitative review of fundamental relationships involved in ablation engineering and aerodynamic heating is presented. This document is written for rapid reading with the primary purpose of introducing the technical area to engineers, scientists, and management personnel associated with but not intimately working in hypervelocity thermal protection.
Provenance: Lockheed Martin Missiles & Fire Control