| LDR | 02166nam a2200373Ma 4500 | ||
| 001 | 011445278 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 100519s1972 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6404970 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)643056300 |
| 040 | ⊔ | ⊔ | ‡aAD# ‡cSTF |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-6707 |
| 088 | ⊔ | ⊔ | ‡aNASA-TN-D-6707 |
| 100 | 1 | ⊔ | ‡aTeren, Fred. |
| 245 | 1 | 0 | ‡aOptimal cruise trajectories for supersonic airplanes / ‡cFred Teren and Carl J. Daniele. |
| 260 | ⊔ | ⊔ | ‡aWashington, DC : ‡bNational Aeronautics and Space Administration, ‡c1972. |
| 300 | ⊔ | ⊔ | ‡a30 p. : ‡bill. ; ‡c26 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vNASA TN D-6707 |
| 500 | ⊔ | ⊔ | ‡a"E-6506." |
| 500 | ⊔ | ⊔ | ‡a"NASA TN D-6707." |
| 500 | ⊔ | ⊔ | ‡a"March 1972." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 22). |
| 520 | ⊔ | ⊔ | ‡aEquations are derived for maximizing range for specified initial and final values of mass and altitude. Constant-velocity flight is assumed, and normal acceleration is neglected. The problem is solved by using the maximum principle. Optimal trajectories are obtained and uniqueness is demonstrated. Results are obtained for a supersonic airplane. Curves are presented which can be used to obtain the optimal trajectory and maximum range for a range of initial and final mass and altitude. The optimal range is compared to the range obtained by using the standard cruise trajectory profile (consisting of a Breguet cruise plus maximum and minimum-thrust connecting segments) and to the range obtained at constant-altitude cruise.--P. [i]. |
| 530 | ⊔ | ⊔ | ‡aAlso available online in PDF from NASA Technical Reports Server Web site. |
| 536 | ⊔ | ⊔ | ‡aSponsored by the National Aeronautics and Space Administration (NASA); performed by the Lewis Research Center under ‡v110-06. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aNumerical analysis. |
| 650 | ⊔ | 0 | ‡aTrajectory optimization. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xTrajectories ‡xMathematical models. |
| 700 | 1 | ⊔ | ‡aDaniele, Carl J. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| 710 | 2 | ⊔ | ‡aLewis Research Center. |
| CID | ⊔ | ⊔ | ‡a011445278 |
| DAT | 0 | ⊔ | ‡a20101111085455.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:36:08Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106883967 ‡y1972 ‡rpd ‡qbib ‡tUS fed doc |