Author

H. P. Kan

Observed names: H. KAN, H.P. Kan, Kan, H. P.

Observed institution: Northrop Grumman (United States)

OpenAlex ID: A5114085964

Compression Fatigue Analysis of Fiber Composites

1981 · M.M. Ratwani, H.P. Kan · Journal of Aircraft · 39

Advanced Certification Methodology for Composite Structures.

1997 · H. P. Kan, R. Cordero, et al. · 32

Enhanced Reliability Prediction Methodology for Impact Damaged Composite Structures

1998 · H. P. Kan · 16

Stress analysis of stepped-lap joints with bondline flaws

1983 · H. P. Kan, M. M. Ratwani · Journal of Aircraft · 15

Analysis of composite-to-metal joints with bondline flaws

1985 · M.M. Ratwani, H.P. Kan · Composites Science and Technology · 10

Nonlinear adhesive behavior effects in cracked metal-to-composite bonded structures

1981 · H.P. Kan, M.M. Ratwani · Engineering Fracture Mechanics · 9

Time-dependent adhesive behavior effects in a stepped lap joint

1982 · M. M. Ratwani, H. P. Kan, et al. · AIAA Journal · 8

Certification Methodology for Stiffener Terminations.

1996 · Chintan Shah, H. P. Kan, et al. · 7

Fatigue sensitivity of composite structure for fighter aircraft

1983 · L.L. Jeans, G.C. Grimes, et al. · Journal of Aircraft · 7

Influence of nonlinear adhesive behavior on analysis of cracked adhesively bonded structures

1980 · M. M. Ratwani, H. P. Kan · AIAA Journal · 7

Compression fatigue analysis of fiber composites

1980 · M. RATWANI, H. KAN · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 7

Certification Testing Methodology for Composite Structure. Volume 2. Methodology Development

1986 · R. S. Whitehead, H. P. Kan, et al. · Defense Technical Information Center (DTIC) · 6

Fatigue sensitivity of composite structure for fighter aircraft

1981 · L. JEANS, G. GRIMES, et al. · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 4

Fatigue crack growth at stress concentrations subjected to strains beyond elastic range

1981 · M. Ratwani, D. P. Wilhem, et al. · Journal of Aircraft · 4

Design Development and Durability Validation of Postbuckled Composite and Metal Panels. Volume 1. Executive Summary

1989 · R. B. Deo, H. P. Kan · 3

Composite patch repair of cracked thick aluminum structures

1984 · H. KAN, M. RATWANI · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 3

Stress analysis of stepped lap joint with bondline flaws

1982 · H. KAN, M. RATWANI · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 3

Growth of Corner Cracks at a Hole

1982 · A. F. Liu, H. P. Kan · Journal of Engineering Materials and Technology · 3

Delamination-based compression residual-strength prediction model for composites

1983 · M. RATWANI, H. KAN · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 2

Statistical modeling of ballistic damage and residual strength in composite structures

1983 · H. KAN, M. RATWANI · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 1

Design Development and Durability Validation of Postbuckled Composite and Metal Panels. Volume 3. Analysis and Test Results

1989 · R. B. Deo, H. P. Kan, et al. · Defense Technical Information Center (DTIC)

Design Development and Durability Validation of Postbuckled Composite and Metal Panels. Volume 4. Design Guide Update

1989 · R. B. Deo, H. P. Kan, et al. · Defense Technical Information Center (DTIC)

Analysis of step-lap joint with weakly bonded regions

1985 · H. KAN, M. RATWANI · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)

Crack-propagation predictions

1977 · H. P. Kan, A. F. Liu, et al. · NASA Tech Briefs

A simple model of dynamic cleavage

1973 · J. M. Anderson, H. P. Kan, et al. · Springer eBooks

Works count: 31

Citation count: 186

H-index: 7

I10-index: 5