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| 035 | ⊔ | ⊔ | ‡asdr-uiuc6369404 |
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| 040 | ⊔ | ⊔ | ‡aBUF ‡cBUF ‡dABC |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3 ‡b.N18 no. 1367 |
| 086 | 0 | ⊔ | ‡aNAS 1.60:1367 |
| 100 | 1 | ⊔ | ‡aAbel, Irving. |
| 245 | 1 | 3 | ‡aAn analytical technique for predicting the characteristics of a flexible wing equipped with an active flutter-suppression system and comparison with wind-tunnel data / ‡cIrving Abel. |
| 260 | ⊔ | ⊔ | ‡a[Washington, D.C.] : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office, ‡c1979. |
| 300 | ⊔ | ⊔ | ‡a42 p. : ‡bill. ; ‡c28 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical paper ; ‡v1367 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aFlutter (Aerodynamics) ‡xMathematical models. |
| 650 | ⊔ | 0 | ‡aOscillating wings (Aerodynamics) ‡xMathematical models. |
| CID | ⊔ | ⊔ | ‡a011427579 |
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| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20241231 ‡sgoogle ‡uuiug.30112101592902 ‡y1979 ‡rpd ‡qbib ‡tUS fed doc |