Add to ORKGThis report presents test results of experiments on the vibration-response characteristics of airplane structures on the ground and in flight. It also gives details regarding the construction and operation of vibration instruments developed by the National Advisory Committee for Aeronautics
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A flight investigation of the spinning of the F4B-2 single-seat fighter airplane was made for the pu...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Measured vibration response of residential structures excited by mechanical and acoustical loading
Accelerations in the lateral and vertical directions were measured at two locations on the floor of ...
This report presents the results of an investigation to determine (1) the magnitude and distribution...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The requirement for low vibrations has achieved the status of a critical design consideration in mod...
An Army liaison-type airplane, representative of personal airplanes in the 150 to 200 horsepower cla...
This report presents test results of experiments on the vibration-response characteristics of airpla...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
The purpose of this test was to collect ground and flight vibration data at Fuselage Station (FS) 50...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A flight investigation of the spinning of the F4B-2 single-seat fighter airplane was made for the pu...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
Ground vibration tests were conducted on a YF-12 airplane. To approximate a structural free-free bou...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Measured vibration response of residential structures excited by mechanical and acoustical loading
Accelerations in the lateral and vertical directions were measured at two locations on the floor of ...
This report presents the results of an investigation to determine (1) the magnitude and distribution...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
The requirement for low vibrations has achieved the status of a critical design consideration in mod...
An Army liaison-type airplane, representative of personal airplanes in the 150 to 200 horsepower cla...
This report presents test results of experiments on the vibration-response characteristics of airpla...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
The purpose of this test was to collect ground and flight vibration data at Fuselage Station (FS) 50...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A flight investigation of the spinning of the F4B-2 single-seat fighter airplane was made for the pu...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...