Add to ORKGPressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted engine nacelles
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...
Force and pressure distribution studies to high angles of attack on all-movable triangular and recta...
Force and pressure measurements on several canopy- fuselage configurations at low supersonic speeds
The present report, which deals with pressure-distribution measurements made on a sweptback wing wit...
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in super...
Supersonic pressure distributions for tip and trailing edge controls on 60 deg delta wing
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted...
From Summary: "Measurements of wing and fuselage pressure distributions were made at low and high su...
The method of determining the pressure distribution on the fuselage is described, with special atten...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution ...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...
Force and pressure distribution studies to high angles of attack on all-movable triangular and recta...
Force and pressure measurements on several canopy- fuselage configurations at low supersonic speeds
The present report, which deals with pressure-distribution measurements made on a sweptback wing wit...
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in super...
Supersonic pressure distributions for tip and trailing edge controls on 60 deg delta wing
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted...
From Summary: "Measurements of wing and fuselage pressure distributions were made at low and high su...
The method of determining the pressure distribution on the fuselage is described, with special atten...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution ...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0
Aerodynamic loads on high-speed aircraft external store adjacent to an unswept wing at mach 0.75 to ...