Roughness effects on boundary-layer transition for blunt-leading-edge plates at Mach 6
Effects of controlled roughness on boundary layer transition for upswept blunted plates in free stream
BLUNT BODY↗
Engineering topics
Holloway, P. F.
Publications and source records attributed to Holloway, P. F..
Application of the pitch modulation maneuver in the region of the ''limiting'' entry velocity.
Pitch modulation maneuver for spacecraft reentry
PITCH CONTROL↗
Definition of lateral-range and lift-drag-ratio requirements for return to both optimum and nonoptimum recovery sites
Lateral range and lift-drag ratio requirements for return to optimum or nonoptimum recovery sites from near-earth circular orbit
LIFT-DRAG RATIO↗
An investigation of heat transfer within regions of separated flow at a Mach number of 6.0
Heat transfer in regions of laminar, transitional, and turbulent separation on sharp and blunt leading edge flat plates at Mach 6.0
HEAT TRANSFER↗
Application of the pitch modulation maneuver in the region of the ''limiting'' entry velocity.
Pitch modulation maneuver for spacecraft reentry
SPACECRAFT REENTRY↗
Effect of controlled surface roughness on boundary-layer transition and heat transfer at mach numbers of 4.8 and 6.0
Effects of controlled surface roughness on boundary layer transition and heat transfer at hypersonic speeds
HYPERSONIC SPEED↗
Effects of controlled roughness on boundary- layer transition at a number of 6.0
Hypersonic boundary layer transition on smooth flat plate with sharp leading edges
FLAT PLATE↗
HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS AT MACH NUMBERS OF 6.0 AND 9.6 OVER TWO REENTRY CONFIGURATIONS FOR THE FIVE-STAGE SCOUT VEHICLE
Heat transfer and pressure distribution over reentry configuration for five-stage scout vehicle
SCOUT LAUNCH VEHICLE↗
EFFECTS OF CONTROLLED ROUGHNESS ON BOUNDARY-LAYER TRANSITION AT A MACH NUMBER OF 6.0
Heat flow rate method used to investigate a hypersonic boundary layer transition on a smooth flat plate with a sharp leading edge
BOUNDARY LAYER TRANSITION↗