High-Performance Supersonic Missile Inlet Design Using Automated Optimization

Collaboration types: Domestic collaboration
Citation topics: 7 Engineering & Materials Science; 7.57 Modelling & Simulation; 7.57.2773 Scramjet
Web Of Science research areas: Engineering, Aerospace
ESI research areas: Engineering

UN Sustainable Development Goals (SDGs)

This output has contributed to the advancement of the following goals:

Source: InCites

Title: High-Performance Supersonic Missile Inlet Design Using Automated Optimization
Creators: Ge-Cheng Zha - Rutgers University
Donald Smith - Rutgers University
Mark Schwabacher - Rutgers University
Khaled Rasheed - Rutgers University
Andrew Gelsey - Rutgers University
Doyle Knight - Rutgers University
Martin Haas - United Technologies Research Center
Publication Details: Journal of aircraft, Vol.34(6), pp.697-705
Academic Unit: College of Engineering; CoE - Mechanical & Aerospace Engineering
Language: English
Resource Type: Journal article
Record Identifier: 991031613437602976