C. M. Hudson
Bio: C. M. Hudson is an academic researcher from Langley Research Center. The author has contributed to research in topics: Fatigue limit & Stress concentration. The author has an hindex of 1, co-authored 1 publications receiving 19 citations.
01 Mar 1970
01 Jan 1974
01 Jun 1976
TL;DR: In this paper, the authors present a bibliography consisting of approximately 1,600 reference citations related to four problem areas in the mechanics of failure in aerospace structures: hydrogen embrittlement, protective coatings, composite materials, and non-destructive evaluation.
Abstract: This bibliography is comprised of approximately 1,600 reference citations related to four problem areas in the mechanics of failure in aerospace structures. The bibliography represents a search of the literature published in the period 1962-1976, the effort being largely limited to documents published in the United States. Listings are subdivided into the four problem areas: Hydrogen Embrittlement; Protective Coatings; Composite Materials; and Nondestructive Evaluation. An author index is included.
TL;DR: In this article, the authors predict the delay in fatigue crack growth and structural life prediction based on compression, creep, stress relaxation, and overloading effects on overloading and stress relaxation.
Abstract: Compression, creep, stress relaxation and overloading effects on delay in fatigue crack growth and structural life predictions
TL;DR: In this paper, the delay period and corresponding crack growth rate transients following overload and overload/underload cycles were systematically measured as a function of load ratio and overload magnitude, and improvements in the model were suggested.
TL;DR: Complex airframe design for economic and safe operation and long life using fatigue and fracture mechanics using fatigue-and fracture-fracture mechanics is discussed in detail in this article.
Abstract: Complex airframe design for economic and safe operation and long life using fatigue and fracture mechanics