A study of the structural-acoustic response and interior noise levels of fuselage structures [PDF]
Models of both flat and curved fuselage panels were tested for their sound transmission characteristics. The effect of external air flow on transmission loss was simulated in a subsonic wind-tunnel. By numerically evaluating the known equations for field-
Koval, L. R.
core +1 more source
Sustainability-Driven Design Optimization of Aircraft Parts Using Mathematical Modeling
The design of aircraft components is a complex process that must simultaneously account for environmental impact, manufacturability, cost and structural performance to meet modern regulatory requirements and sustainability objectives.
Aikaterini Anagnostopoulou +3 more
doaj +1 more source
Aerodynamic preliminary analysis system 2. Part 2: User's manual [PDF]
An aerodynamic analysis system based on potential theory at subsonic and/or supersonic speeds and impact type finite element solutions at hypersonic conditions is described.
Divan, P., Sova, G., Spacht, L.
core +1 more source
Damage tolerance analysis of aircraft reinforced panels [PDF]
This work is aimed at reproducing numerically a campaign of experimental tests performed for the development of reinforced panels, typically found in aircraft fuselage.
A. Pirondi, F. Carta
doaj
Local stiffener and skin pocket buckling prediction by special PASCO modeling technique: Correlation to test data [PDF]
Waffle panels are often used on fuselage structures such as that of the Space Shuttle. The waffle panel design is an efficient design for carrying biaxial, in-plane, and shear loads. The WAFFLE program was designed for application on waffle panels.
Swift, Patrick M. +2 more
core +1 more source
Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft [PDF]
The use of Helmholtz resonators to increase the sidewall transmission loss (TL) in aircraft cabin sidewalls is evaluated. Development, construction, and test of an aircraft cabin acoustic enclosure, built in support of the Propfan Test Assessment (PTA ...
Balena, F. J. +3 more
core +1 more source
On the application of population-based structural health monitoring in aerospace engineering. [PDF]
Brennan DS +4 more
europepmc +1 more source
Development of MCAERO wing design panel method with interactive graphics module [PDF]
A reliable and efficient iterative method has been developed for designing wing section contours corresponding to a prescribed subcritical pressure distribution.
Bristow, D. R., Hawk, J. D.
core +1 more source
Design and manufacture of a reinforced fuselage structure through automatic laying-up and in-situ consolidation with co-consolidation of skin and stringers using thermoplastic composite materials. [PDF]
Martín I +5 more
europepmc +1 more source
Aircraft interior noise reduction by alternate resonance tuning [PDF]
Model problem development and analysis continues with the Alternate Resonance Tuning concept. Various topics are presently at different stages of completion and are described.
Bliss, Donald B., Gottwald, James A.
core +7 more sources

