Development of a Premixed Combustion Capability for Dual-Mode Scramjet Experiments [0.03%]
用于双模 scramjet实验的预混燃烧能力的发展研究
Robert D Rockwell,Christopher P Goyne,Harsha Chelliah et al.
Robert D Rockwell et al.
Hypersonic air-breathing engines rely on scramjet combustion processes, which involve high-speed, compressible, and highly turbulent reacting flows. The combustion environment and the turbulent flames at the heart of these engines are diffi...
James E Polk,Anthony Pancotti,Thomas Haag et al.
James E Polk et al.
Accurate, direct measurement of thrust or impulse is one of the most critical elements of electric thruster characterization, and one of the most difficult measurements to make. This paper summarizes recommended practices for the design, ca...
Infrared Signature Suppression of Helicopter Engine Duct Based on "Conceal and Camouflage" [0.03%]
基于“隐蔽伪装”的直升机发动机进气道红外特征抑制
Mahulikar, Shripad P.; Prasad, Subramanya; Potnuru et al.
Mahulikar et al.
CAMPBELL, W. H.; KO, B. N.; LOWE et al.
CAMPBELL et al.
Numerical Investigation of the Supersonic Combustion of Kerosene in a Strut-Based Combustor [0.03%]
支柱式燃烧器中煤油超音速燃烧的数值研究
Kumaran, K; Behera, Prabhat Ranjan; Babu et al.
Kumaran et al.
Hedges, D. E.; Meserole, J. S.
Hedges
Pfeiffer, Jens; Kuehl, Hans-Detlev
Pfeiffer
Mitani, Tohru; Tani, Kouichiro; Miyajima et al.
Mitani et al.
Demayo, T. N.; Leong, M. Y.; Samuelsen et al.
Demayo et al.
Ebrahimi, Houshang B.; Merkle, Charles L.
Ebrahimi