Add to ORKGThis report describes an electrical hinge-moment balance for use with wind-tunnel models of aircraft. A brief description of the principle of operation and operating experience with the balance is given in part I. Part II gives constructional details and part III gives theoretical considerations. Extensive constructional information is given to enable the reproduction of the equipment
Abstract: Starting from the German experience in the field of electrical measurement of mechanical ...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynami...
Given here is a description of the design of a scientific recording wind tunnel balance. It was deci...
The elevator hinge moment of N219-B12 was investigated based on the design criteria corres...
A 1/12-scale model of a horizontal tail of a fighter airplane was tested through the transonic speed...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
This report combines the wind-tunnel results of tests on four control surface models made in the two...
Various wind-tunnel data on the hinge-moment characteristics of control-surface tabs have been colle...
An investigation was made in the LWAL 7- by 10-foot tunnel of internally balanced, sealed ailerons f...
This is a copy of the author 's preprint version of an article published in the journal Experimental...
An investigation of the elevator and rudder hinge moment parameters of an aircraft obtained by analy...
M.Phil.In today's world with its competitive environment there is a need to shorten product developm...
Wind tunnel measurements of the aerodynamic loads acting on two store configurations supported in th...
Abstract: Starting from the German experience in the field of electrical measurement of mechanical ...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynami...
Given here is a description of the design of a scientific recording wind tunnel balance. It was deci...
The elevator hinge moment of N219-B12 was investigated based on the design criteria corres...
A 1/12-scale model of a horizontal tail of a fighter airplane was tested through the transonic speed...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
This report combines the wind-tunnel results of tests on four control surface models made in the two...
Various wind-tunnel data on the hinge-moment characteristics of control-surface tabs have been colle...
An investigation was made in the LWAL 7- by 10-foot tunnel of internally balanced, sealed ailerons f...
This is a copy of the author 's preprint version of an article published in the journal Experimental...
An investigation of the elevator and rudder hinge moment parameters of an aircraft obtained by analy...
M.Phil.In today's world with its competitive environment there is a need to shorten product developm...
Wind tunnel measurements of the aerodynamic loads acting on two store configurations supported in th...
Abstract: Starting from the German experience in the field of electrical measurement of mechanical ...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...