publication . Article . Conference object . 1971

Jet noise excitation of an integrally stiffened panel

M.D. Olson; Garry M. Lindberg;
  • Published: 21 Jun 1971
  • Publisher: American Institute of Aeronautics and Astronautics
Abstract
1 Shanley, F., Weight Strength Analysis of Aircraft Structures, 1st ed., McGraw-Hill, New York, 1952; 2nd ed., Dover, New York, 1960. 2 Vinson, J. R. and Shore, S., "Bibliography on Methods of Structural Optimization for Flat Sandwich Panels," NAECASL-1082, April 1965, Naval Air Engineering Center, Philadelphia, Pa. 3 Vinson, J. R. and Shore, S., "Methods of Structural Optimization for Flat Sandwich Panels," NAEC-ASL-1083, April 1965, Naval Air Engineering Center, Philadelphia, Pa. 4 Vinson, J. R. and Shore, S., "Design Procedures for the Structural Optimization of Flat Sandwich Panels," NAECASL-1084, April 1965, Naval Air Engineering Center, Philadelphia, Pa. 5...
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Persistent Identifiers

doi: 10.2514/6.1971-585 , 10.2514/3.59181

Subjects
free text keywords: Aerospace Engineering, Acoustics, Physics, Excitation, Integrally closed, Jet noise, Government printing office, Engineering, business.industry, business, Aerospace, Shore, geography.geographical_feature_category, geography, Sandwich-structured composite, Uniaxial compression, Truss, Structural engineering
Related Organizations
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Journal of Aircraft
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https://doi.org/10.2514/6.1971...
Conference object . 1971
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