JAMES R. STERRETT

Effect of controlled surface roughness on boundary-layer transition and heat transfer at mach numbers of 4.8 and 6.0

P. F. Holloway, JAMES R. STERRETT · NASA Technical Reports Server (NASA) · 1964 · 56 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Flow field for sonic jet exhausting counter to a hypersonic mainstream

David J. Romeo, JAMES R. STERRETT · AIAA Journal · 1965 · 37 citations

Engineering, Aerospace Engineering, Mechanical Engineering +16

EFFECTS OF CONTROLLED ROUGHNESS ON BOUNDARY-LAYER TRANSITION AT A MACH NUMBER OF 6

P. F. Holloway, JAMES R. STERRETT · AIAA Journal · 1963 · 29 citations

Engineering, Aerospace Engineering, Physics +13

An investigation of heat transfer within regions of separated flow at a Mach number of 6.0

H. S. Creekmore, P. F. Holloway, JAMES R. STERRETT · NASA Technical Reports Server (NASA) · 1965 · 28 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

A theoretical and experimental investigation of secondary jets in a Mach 6 free stream with emphasis on the structure of the jet and separation ahead of the jet

Jennie Barber, JAMES R. STERRETT · NASA Technical Reports Server (NASA) · 1966 · 20 citations · Full text

Engineering, Aerospace Engineering, Physics +17