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035 a| (Sirsi) o844605587;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:110331;

100 1 a| Cvitkovich, Michael,e| author.?| UNAUTHORIZED;

245 10 a| Fatigue debonding characterization in composite skin/stringer configurations /c| Michael K. Cvitkovich, T. Kevin O'Brien, Pierre J. Minguet.;

300 a| 1 online resource (33 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 110331;

490 1 a| U. S. Army Research Laboratory technical report ;v| ARL-TR-1342;

500 a| "April 1997.";

500 a| Technical memo., Prepared in collaboration with the Boeing Defense and Space Group, Philadelphia, PA. Errata: Page 13, Table 2: Column 2 heading should read E sub 22 GPa.;

500 a| "Performing organization: NASA Langley Research Center"--Report documentation page.;

500 a| CRDP Program record.;

504 a| Includes bibliographical references (page 12).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| 581-10-21-01;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Apr. 5, 2017).;

650 7 a| Fatigue tests.2| nasat;

650 7 a| Debonding (Materials)2| nasat;

650 7 a| Composite structures.2| nasat;

650 7 a| Flanges.2| nasat;

650 7 a| Skin (Structural member)2| nasat;

650 7 a| Bonded joints.2| nasat;

650 7 a| Crack initiation.2| nasat;

650 7 a| Delaminating.2| nasat;

650 7 a| Graphite-epoxy composites.2| nasat;

650 7 a| Resin matrix composites.2| nasat;

700 1 a| O'Brien, T. Kevin,e| author.=| ^A430485;

700 1 a| Minguet, Pierre Jacques,e| author.?| UNAUTHORIZED;

710 1 a| United States.b| Army Materiel Command.=| ^A379010;

710 2 a| Langley Research Center,e| issuing body.=| ^A192893;

776 08 i| Print version:t| Fatigue Debonding Characterization in Composite Skin/Stringer Configurationsw| (OCoLC)45531880;

776 08 i| Microfiche version:a| Cvitkovich, Michael K.t| Fatigue debonding characterization in composite skin/stringer configurationsw| (OCoLC)38846908;

830 0 a| NASA technical memorandumv| 110331.=| ^A467613;

830 0 a| ARL-TR (Aberdeen Proving Ground, Md.) ;v| 1342.=| ^A566074;

856 40 u| https://purl.fdlp.gov/GPO/gpo65166;

949 a| Click on web addressw| asish| joyner94;

998 a| 4694672;

998 a| u4694672;

596 a| 1;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4694672-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 5/15/2017x| EDOCUMENTz| JERESOURCE;

Fatigue debonding characterization in composite skin/stringer configurations / Michael K. Cvitkovich, T. Kevin O'Brien, Pierre J. Minguet.

Author/creator	Cvitkovich, Michael author.
Format	Electronic
Publication	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center ; Alexandria, Virginia : U.S. Army Materiel Command, April 1997.
Description	1 online resource (33 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo65166

Other author/creator	O'Brien, T. Kevin, author.
Other author/creator	Minguet, Pierre Jacques, author.
Other author/creator	United States. Army Materiel Command.
Other author/creator	Langley Research Center, issuing body.
Series	NASA technical memorandum ; 110331 U. S. Army Research Laboratory technical report ; ARL-TR-1342 NASA technical memorandum 110331. ^A467613 ARL-TR (Aberdeen Proving Ground, Md.) ; 1342. ^A566074
General note	"April 1997."
General note	Technical memo., Prepared in collaboration with the Boeing Defense and Space Group, Philadelphia, PA. Errata: Page 13, Table 2: Column 2 heading should read E sub 22 GPa.
General note	"Performing organization: NASA Langley Research Center"--Report documentation page.
General note	CRDP Program record.
Bibliography note	Includes bibliographical references (page 12).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration 581-10-21-01
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Apr. 5, 2017).
Issued in other form	Print version: Fatigue Debonding Characterization in Composite Skin/Stringer Configurations
Issued in other form	Microfiche version: Cvitkovich, Michael K. Fatigue debonding characterization in composite skin/stringer configurations
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:110331

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Fatigue debonding characterization in composite skin/stringer configurations / Michael K. Cvitkovich, T. Kevin O'Brien, Pierre J. Minguet.

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