Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Derrick Alexander"'
Autor:
POPE, DERRICK ALEXANDER
Publikováno v:
Georgia Bar Journal; May2024, Vol. 29 Issue 5, p40-47, 7p
Autor:
POPE, DERRICK ALEXANDER
Publikováno v:
Georgia Bar Journal; Dec2023, Vol. 29 Issue 3, p30-39, 9p
Autor:
POPE, DERRICK ALEXANDER
Publikováno v:
Georgia Bar Journal; Jun2022, Vol. 27 Issue 6, p16-25, 12p
Autor:
Grant Ingram, William D. E. Allan, Robert Stowe, Asad Asghar, Marc LaViolette, Derrick Alexander
Publikováno v:
Volume 1: Aircraft Engine; Fans and Blowers; Marine.
This paper reports the internal performance evaluation of S-duct diffusers with different offset-to-length ratios. The geometric parameters of S-duct diffusers are currently of great interest because of increasing demand for stealth and consequently,
Autor:
Pierre Fournier, Richard Link, Robert Stowe, Tracy Smithson, Rogerio Pimentel, Derrick Alexander, Sophie Ringuette
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 14:29-56
Publikováno v:
Volume 1: Aircraft Engine; Fans and Blowers; Marine.
This paper reports the internal performance evaluation of S-duct diffusers with different entrance aspect ratios as part of an ongoing parametric investigation of a generic S-duct inlet. The generic S-duct diffusers were a rectangular-entrance (aspec
Autor:
Derrick, Alexander
Aluminum magnesium alloys, due to their high strength and overall corrosion resistance, are used more and more in a variety of applications, from automobiles to navy ships. The addition of magnesium greatly increases the strength of aluminum. However
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::993f4aa22b58a1f92ccb2ab76599dabb
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 11:487-510
Publikováno v:
Journal of Propulsion and Power. 26:1125-1134
The aeropropulsive performance characteristics of a scramjet and a shock-induced combustion ramjet (shcramjet) are compared at a flight Mach number of 11 and an altitude of 34.5 km. The vehicles share the same inlet type, fuel injection system, fuel/
Autor:
Derrick Alexander, Jean P. Sislian
Publikováno v:
Journal of Propulsion and Power. 24:34-44
A shock-induced combustion ramjet is considered wherein gaseous hydrogen is injected via cantilevered ramp injectors located in a staggered manner on opposite walls of the internal duct of a mixed-compression inlet. The nonhomogeneous combustible mix