Add to ORKGTests were carried out on 20 inch x 20 inch panels at different test conditions using free-free pane...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Structural borne interior noise in a single engine general aviation aircraft was studied to determin...
Vibration effects of simple curved panels to high intensity random and discrete frequency nois
Sonic fatigue effects on structural reliability of randomly excited aluminum viscoelastic panels at ...
An experimental study to determine the acoustic fatigue characteristics of a flat multi-layered stru...
A number of aircraft and spacecraft configurations are being considered for future development. Thes...
Lightweight aircraft structures exposed to a high intensity noise environment can fatigue prematurel...
Analytical models and computer programs for structural response calculations under action of mechani...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
Summarized are the progress and accomplishments performed under NASA/Langley Research Center Master ...
"NASA TN D-1.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...
The reduction of interior noise in light aircraft was investigated with emphasis the thin fuselage s...
Models of both flat and curved fuselage panels were tested for their sound transmission characterist...
The related literature was reviewed and a preliminary analytical model was developed for simplified ...
Tests were carried out on 20 inch x 20 inch panels at different test conditions using free-free pane...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Structural borne interior noise in a single engine general aviation aircraft was studied to determin...
Vibration effects of simple curved panels to high intensity random and discrete frequency nois
Sonic fatigue effects on structural reliability of randomly excited aluminum viscoelastic panels at ...
An experimental study to determine the acoustic fatigue characteristics of a flat multi-layered stru...
A number of aircraft and spacecraft configurations are being considered for future development. Thes...
Lightweight aircraft structures exposed to a high intensity noise environment can fatigue prematurel...
Analytical models and computer programs for structural response calculations under action of mechani...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
Summarized are the progress and accomplishments performed under NASA/Langley Research Center Master ...
"NASA TN D-1.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...
The reduction of interior noise in light aircraft was investigated with emphasis the thin fuselage s...
Models of both flat and curved fuselage panels were tested for their sound transmission characterist...
The related literature was reviewed and a preliminary analytical model was developed for simplified ...
Tests were carried out on 20 inch x 20 inch panels at different test conditions using free-free pane...
Calculation methods for vibration responses of spacecraft structural members to acoustic field
Structural borne interior noise in a single engine general aviation aircraft was studied to determin...