Design for minimum weight. Compression panels with unflanged integral stiffeners having dimensional restrictions.
Abstract:ESDU 70007 gives the cross-sectional dimensions for minimum weight of uniform compression panels having unflanged integral stiffeners. Data are also given for determining the dimensions of the panel of least weight when one or more of the cross-sectional dimensions is fixed or restricted. An allowance is made for the effects of initial irregularities and plasticity correction factors are included.
|Data Item ESDU 70007|
- Aircraft Noise
- Fatigue - Endurance Data
- Fatigue - Fracture Mechanics
- Fluid Mechanics, Internal Flow
- Fluid Mechanics, Internal Flow (Aerospace)
- Heat Transfer
- Physical Data, Chemical Engineering
- Stress and Strength
- Transonic Aerodynamics
- Vibration and Acoustic Fatigue
- Wind Engineering
Aerospace Materials Data
Additional Engineering References