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

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

著者名:

Newman, J.C., Jr. ( NASA Langley Research Center )
Crews, J.H.. Jr.
Bigelow, C.A.
Dawicke, D.S.

掲載資料名:

NASA Technical Reports

発行年:

1994

号:

NASA-TM-109119

パート:

NAS 1.15:109119

ペーパー番号:

N94-34385

開始ページ:

1

終了ページ:

29

総ページ数:

29

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00001430

類似資料:

1 テクニカルペーパー Three-Dimensional CTOA and Constraint Effects During Stable Tearing in a Thin-Sheet Material Dawicke, D.S., Newman, J.C., Bigelow, C.A. National Aeronautics and Space Adminstration	7 テクニカルペーパー The Nonlinear Response of Cracked Aluminum Shells Subjected to Combined Loads Rose,C.A., Young,R.D., Starnes Jr.,J.H. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー MEASUREMENT AND ANALYSIS OF CRITICAL CTOA FOR AN ALUMINUM ALLOY SHEET Dawicke, D.S., Sutton, M.A., Nerman, J.C. ,Jr., Bigelow, C.A. National Aeronautics and Space Adminstration	8 テクニカルペーパー Computer simulation of elastic stress analyses of two-dimensional multiple-cracked bodies Newman, J.C., Jr., Mear, M.E., Raju, I.S. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー STRESS-INTENSITY FACTORS FOR CIRCUMFERENTIAL SURFACE CRACKS IN PIPES AND RODS UNDER TENSION AND BENDING LOADS Raju, I. S., Newman, Jr., J. C. National Aeronautics and Space Administration	9 テクニカルペーパー Orientation effects on the measurement and analysis of critical CTOA in an aluminum alloy sheet Sutton, M. A., Dawicke, D. S., Newman, J. C., Jr. National Aeronautics and Space Adminstration
4 テクニカルペーパー THROUGH-THE-THICKNESS FATIGUE CRACK CLOSURE BEHAVIOR IN AN ALUMINUM ALLOY Dawicke, D.S., Newman, J.C.,Jr., Grandt, A.F.,Jr. National Aeronautics and Space Adminstration	10 テクニカルペーパー Stress concentrations for straight-shank and countersunk holes in plates subjected to tension, bending, and pin loading Shivakumar, K. N., Newman, J. C., Jr. National Aeronautics and Space Adminstration
5 テクニカルペーパー Stable Tearing Behavior of a Thin-Sheet Material with Multiple Cracks Dawicke, D.S., Newman, J.C., Sutton, M.A., Jr., Amstutz, B.E. National Aeronautics and Space Adminstration	11 テクニカルペーパー ZIP3D - AN ELASTIC AND ELASTIC-PLASTIC FINITE-ELEMENT ANALYSIS PROGRAM FOR CRACKED BODIES Shivakumar, K.N., Newman, J.C., Jr. National Aeronautics and Space Adminstration
6 テクニカルペーパー 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. National Aeronautics and Space Adminstration	12 テクニカルペーパー EFFECT OF DEBOND GROWTH ON STRESS-INTENSITY FACTORS IN A CRACKED ORTHOTROPIC SHEET STIFFENED BY A SEMI-INFINITE Bigelow, C.A. National Aeronautics and Space Administration

1

2

3

4

5

6

7

8

9

10

11

12