Work

Numerical study of a transpiration cooled rocket nozzle

Year: 1996

Type: conference-paper

Source: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

DOI: 10.2514/6.1996-2580

Authors: Jay Landis, W. Bowman

Institution: U.S. Air Force Institute of Technology

Language: English

Topic: Rocket and propulsion systems research

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Aeronautics and Space Administration

OpenAlex ID: W1967332147

FWCI: 2.204

Cites: 8

Cited by: 44

Related to: 10