Add to ORKGTransonic aerodynamic characteristics of two-stage fin-stabilized rocket launch vehicle in combination with winged spacecraf
Results from analytical and experimental studies of the aerodynamic characteristics of a turbojet-bo...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
An experimental investigation was conducted to provide a systematic set of lateral-directional stabi...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
A proposed wing body reusable launch vehicle was tested in the Marshall Space Flight Center (MSFC) 1...
Pressure and load distributions for a related group of simulated launch vehicle configurations are p...
The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable laun...
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback lea...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
The aeropropulsive characteristics of an advanced fighter designed for supersonic cruise were determ...
Experimental tests have been conducted to determine possible aerodynamic interference effects due to...
Tests were conducted at Mach numbers of 3.96 and 4.65 in the Langley Unitary Plan wind tunnel to det...
The circular body configuration is a generic single- or multi-stage reusable Earth-to-orbit transpor...
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
Results from analytical and experimental studies of the aerodynamic characteristics of a turbojet-bo...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
An experimental investigation was conducted to provide a systematic set of lateral-directional stabi...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
A proposed wing body reusable launch vehicle was tested in the Marshall Space Flight Center (MSFC) 1...
Pressure and load distributions for a related group of simulated launch vehicle configurations are p...
The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable laun...
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback lea...
Effect of rearward body strakes on transonic aerodynamic characteristics of unswept-wing fighter air...
The aeropropulsive characteristics of an advanced fighter designed for supersonic cruise were determ...
Experimental tests have been conducted to determine possible aerodynamic interference effects due to...
Tests were conducted at Mach numbers of 3.96 and 4.65 in the Langley Unitary Plan wind tunnel to det...
The circular body configuration is a generic single- or multi-stage reusable Earth-to-orbit transpor...
This report presents the results of an investigation conducted in the Langley 300 mph 7- by 10-foot ...
Results from analytical and experimental studies of the aerodynamic characteristics of a turbojet-bo...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
An experimental investigation was conducted to provide a systematic set of lateral-directional stabi...