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Technical Paper

1. Computer simulation of elastic stress analyses of two-dimensional multiple-cracked bodies

Newman, J.C., Jr. ; Mear, M.E. ; Raju, I.S.

Pub. info.:	A collection of technical papers : 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, April 15-17, 1996, Salt Lake City, UT. pt. 2 pp.869-876, 1996. Washington, DC. American Institute of Aeronautics and Astronautics
Title of ser.:	AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Ser. no.:	CP962

Technical Paper

2. An Extended Compact Tension Specirnen for Fatigue Crack Propagation and Fracture

Piascik, R.S. ; Newman, J.C., Jr.

Pub. info.:

NASA Technical Reports. 19960021053 (NASA-TM-110243), pp.1-18, 1996. National Aeronautics and Space Adminstration

Technical Paper

3. AN EVALUATIONN OF THE PRESSURE PROOF TEST CONCEPT FOR THIN SHEET 2024-T3

Dawicke, D.S. ; Poe, C.C., Jr. ; Newman, J.C., Jr. ; Harris, C.E.

Pub. info.:

NASA Technical Reports. (NASA-TM-101675), pp.1-32, 1990. National Aeronautics and Space Adminstration

Technical Paper

4. FASTRAN-II- A FATIGUE CRACK GROWTH STRUCTURAL ANALYSIS PROGRAM

Newman, J.C., Jr.

Pub. info.:

NASA Technical Reports. (NASA-TM-104159), pp.1-104, 1992. National Aeronautics and Space Adminstration

Technical Paper

5. ZIP3D - AN ELASTIC AND ELASTIC-PLASTIC FINITE-ELEMENT ANALYSIS PROGRAM FOR CRACKED BODIES

Shivakumar, K.N. ; Newman, J.C., Jr.

Pub. info.:

NASA Technical Reports. (NASA-TM-102753), pp.1-102, 1990. National Aeronautics and Space Adminstration

Technical Paper

6. FATIGUE CRACK INITIATION AND SMALL CRACK GROUTH ON SEVERAL AIRFRAME ALLOYS

Swin, M.H. ; Newman, J.C., Jr. ; Phillips, E.P.

Pub. info.:

NASA Technical Reports. (NASA-TM-102598), pp.1-8, 1990. National Aeronautics and Space Adminstration

Technical Paper

7. Small-Crack Effects in High-Strength Aluminum Alloys

Newman, J.C., Jr. ; Wu, X.R. ; Venneri, S.L. ; Li, C.G.

Pub. info.:

NASA Technical Reports. (NASA-RP-1309), pp.1-116, 1994. National Aeronautics and Space Adminstration

Technical Paper

8. Variations of a Global Constraint Factor in Cracked Bodies Under Tension and Bending Loads

Newman, J.C., Jr. ; Crews, J.H.. Jr. ; Bigelow, C.A. ; Dawicke, D.S.

Pub. info.:

NASA Technical Reports. (NASA-TM-109119), pp.1-29, 1994. National Aeronautics and Space Adminstration

Technical Paper

9. surf3d: A 3D FINITE-ELEMENT PROGRAM FOR THE ANALYSIS OF SURFACE AND CORNER CRACKS IN SOLIDS SUBJECTED TO MODE-I LOADINGS

RAJU, I.S. ; Newman, J.C., Jr.

Pub. info.:

NASA Technical Reports. (NASA-TM-107710), pp.1-101, 1993. National Aeronautics and Space Adminstration

10.

Technical Paper

10. PREDICTION OF STABEL TEARING OF 2024-T3 ALUMINUM ALLOY USING THE CRACK-TIP OPENING ANGLE APPROACH

Bakuckas, J.G., Jr. ; Newman, J.C., Jr.

Pub. info.:

NASA Technical Reports. (NASA-TM-109023), pp.1-24, 1993. National Aeronautics and Space Adminstration

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