Add to ORKGAt the request of the Henschel Aircraft Works. A. G. Berlin. three models of the missile "Zitterrochen" were investigated at subsonic velocities.(open jet 215-millimeter diameter) and at supersonic velocities (open jet 110 by 130 millimeters) in order to determine the effect of various wing forms on the air forces and moments. Three-component measurements were taken, and one model was also investigated with deflected control plates
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon conf...
The effects of external fuel tanks and externally mounted rocket packets on the drag characteristics...
At the request of the Henschel Aircraft Works. A. G. Berlin. three models of the missile "Zitterroch...
An investigation has been made in the Langley 9- by 12-inch super-sonic blowdown tunnel at Mach numb...
A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without...
Wind tunnel test results of an Anti-Tank Missile model with five different warheads are presented in...
Tests of an airplane model equipped with missiles were made to inves-An evaluation of pylons suitabl...
A low-speed wind-tunnel investigation has been made of some aspects of the aerodynamic problems asso...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine th...
The Air Force Research Laboratory\u27s Munitions Directorate has been looking to extend the range of...
In the process of missile design, the aerodynamic characteristics of missile as an important factor ...
Documentation and interpretation of experimental results obtained from force and moment measurements...
Wind-tunnel measurements on projectiles are discussed. Tests at the Gottingen Tunnel are described. ...
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon conf...
The effects of external fuel tanks and externally mounted rocket packets on the drag characteristics...
At the request of the Henschel Aircraft Works. A. G. Berlin. three models of the missile "Zitterroch...
An investigation has been made in the Langley 9- by 12-inch super-sonic blowdown tunnel at Mach numb...
A wind-tunnel investigation was carried out on an oscillating model of the F-5 wing with and without...
Wind tunnel test results of an Anti-Tank Missile model with five different warheads are presented in...
Tests of an airplane model equipped with missiles were made to inves-An evaluation of pylons suitabl...
A low-speed wind-tunnel investigation has been made of some aspects of the aerodynamic problems asso...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine th...
The Air Force Research Laboratory\u27s Munitions Directorate has been looking to extend the range of...
In the process of missile design, the aerodynamic characteristics of missile as an important factor ...
Documentation and interpretation of experimental results obtained from force and moment measurements...
Wind-tunnel measurements on projectiles are discussed. Tests at the Gottingen Tunnel are described. ...
Tests were conducted in the Aerodynamic Wind Tunnel (4T) to evaluate the validity of weapon aerodyna...
Exploratory static-stability tests were made on models of the MK-84 weapon and a modular weapon conf...
The effects of external fuel tanks and externally mounted rocket packets on the drag characteristics...