Add to ORKGJet pluming effect on static stability of five cone cylinder-flare finned rocket models at Mach numbers of 4, 5, and 6 and static pressure ratios up to 26,00
Static longitudinal stability and control characteristics of wingless missile configuration at super...
Pressure distribution on base and afterbody of missile configuration with and without jet flow using...
Jet-plume-induced flow separation on asymmetric bodies at 3.00, 4.50, and 6.00 Mach number
Effects of jet pluming on static stability of ballistic bodies at Mach number of 6.0
Simulated rocket jet exhaust effect on stability and control of research aircraft configuratio
Static stability of single-stage meteorological sounding rocket at Mach numbers from 6.0 to 12.
Cover title."September 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion ...
Static stability of sounding rocket at Mach numbers 1.50 to 4.63 to determine effect of body length ...
Measurements have been made in air at two Mach numbers of the static stability, normal force, and dr...
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteri...
Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liqui...
The effect of plume-induced flow separation and aspiration effects due to operation of both orbiter ...
A theoretical investigation was conducted to determine the effects of body boundary-layer separation...
Static stability characteristics of preliminary models of X-15 research aircraft at supersonic speed
Jet plume induced, flow separation on lifting entry model flat bottom by pressure distribution analy...
Static longitudinal stability and control characteristics of wingless missile configuration at super...
Pressure distribution on base and afterbody of missile configuration with and without jet flow using...
Jet-plume-induced flow separation on asymmetric bodies at 3.00, 4.50, and 6.00 Mach number
Effects of jet pluming on static stability of ballistic bodies at Mach number of 6.0
Simulated rocket jet exhaust effect on stability and control of research aircraft configuratio
Static stability of single-stage meteorological sounding rocket at Mach numbers from 6.0 to 12.
Cover title."September 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Propulsion ...
Static stability of sounding rocket at Mach numbers 1.50 to 4.63 to determine effect of body length ...
Measurements have been made in air at two Mach numbers of the static stability, normal force, and dr...
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteri...
Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liqui...
The effect of plume-induced flow separation and aspiration effects due to operation of both orbiter ...
A theoretical investigation was conducted to determine the effects of body boundary-layer separation...
Static stability characteristics of preliminary models of X-15 research aircraft at supersonic speed
Jet plume induced, flow separation on lifting entry model flat bottom by pressure distribution analy...
Static longitudinal stability and control characteristics of wingless missile configuration at super...
Pressure distribution on base and afterbody of missile configuration with and without jet flow using...
Jet-plume-induced flow separation on asymmetric bodies at 3.00, 4.50, and 6.00 Mach number