The nature of some cases of flow separation, flow-field interference, unusual vehicle shape or size,...
An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...
Measurements have been made in air at two Mach numbers of the static stability, normal force, and dr...
Static stability of sounding rocket at Mach numbers 1.50 to 4.63 to determine effect of body length ...
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback lea...
Sounding rockets are rocket vehicles designed to carry scientific payloads above the sensible level ...
Jet pluming effect on static stability of five cone cylinder-flare finned rocket models at Mach numb...
Two rocket models having cruciform, aspect-ratio-5, unwswept tails and a fineness-ratio-20 fuselage ...
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteri...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Measurements of lift, drag and pitching moment have been made in the. No. lA Wind Tunnel at the Col...
Static aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low tu...
Static longitudinal stability and control characteristics of air-to-surface canard missile configura...
An investigation of the static and dynamic longitudinal stability characteristics of 1/3.7 scale roc...
Tests were conducted at Mach numbers of 3.96 and 4.65 in the Langley Unitary Plan wind tunnel to det...
The nature of some cases of flow separation, flow-field interference, unusual vehicle shape or size,...
An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...
Measurements have been made in air at two Mach numbers of the static stability, normal force, and dr...
Static stability of sounding rocket at Mach numbers 1.50 to 4.63 to determine effect of body length ...
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback lea...
Sounding rockets are rocket vehicles designed to carry scientific payloads above the sensible level ...
Jet pluming effect on static stability of five cone cylinder-flare finned rocket models at Mach numb...
Two rocket models having cruciform, aspect-ratio-5, unwswept tails and a fineness-ratio-20 fuselage ...
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteri...
The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determ...
Measurements of lift, drag and pitching moment have been made in the. No. lA Wind Tunnel at the Col...
Static aerodynamic characteristics of three-stage trailblazer ii rocket vehicle determined in low tu...
Static longitudinal stability and control characteristics of air-to-surface canard missile configura...
An investigation of the static and dynamic longitudinal stability characteristics of 1/3.7 scale roc...
Tests were conducted at Mach numbers of 3.96 and 4.65 in the Langley Unitary Plan wind tunnel to det...
The nature of some cases of flow separation, flow-field interference, unusual vehicle shape or size,...
An investigation at medium to high subsonic speeds has been conducted in the Langley low-turbulence ...
Measurements have been made in air at two Mach numbers of the static stability, normal force, and dr...