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The mechanism of the fuel-mixing process in diffusion-type supersonic combustion /Watton, Alan January 1968 (has links)
No description available.
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Numerical investigation of wing morphing capabilities applied to a Horten type swept wing geometryVishwanathan, Ashwin. January 2007 (has links)
Thesis (M.S.)--West Virginia University, 2007. / Title from document title page. Document formatted into pages; contains viii, 58 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 51-52).
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Improvement of the performance of a turbo-ramjet engine for UAV and missile applications /Krikellas, Dimitrios. January 2003 (has links) (PDF)
Thesis (M.S. in Applied Physics and M.S. in Aeronautical Engineering)--Naval Postgraduate School, December 2003. / Thesis advisor(s): Garth V. Hobson, Kai E. Woehler. Includes bibliographical references (p. 133). Also available online.
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Effects of displays and alerts on subject reactions to potential collisions during closely spaced parallel approachesVandor, Balazs 12 1900 (has links)
No description available.
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Finite-state inflow applied to aeroelastic flutter or fixed and rotating wingsNibbelink, Bruce D. 05 1900 (has links)
No description available.
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66 |
Integration of unigraphics and cost advantage for aircraft engine parts configuarationChintamaneni, Prashantkumar. January 2000 (has links)
Thesis (M.S.)--Ohio University, March, 2000. / Title from PDF t.p.
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67 |
Airplane dynamic modeling and automatic flight control design /Wolfe, Douglas E., January 1990 (has links)
Project report (M.S.)--Virginia Polytechnic Institute and State University, 1990. / Vita. Abstract. Includes bibliographical references (leaf 59). Also available via the Internet.
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The use of plywood in airplane wing beamsHeck, George Emil. January 1925 (has links)
Thesis (M.S.)--University of Wisconsin, 1925. / eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.
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Identification of human factors concerns in joint strike fighter and training recommendations /Bitik, Arif B. Kueluenk, Buelent. January 2008 (has links) (PDF)
Master's Thesis (M.S. in Modeling, Virtual Environments, and Simulation (MOVES))--Naval Postgraduate School, September 2008. / Title from reproduction cover. "September 2008." Thesis advisors: Joseph Sullivan, Michael McCauley, and Anthony Ciavarelli. Performed by Naval Postgraduate School, Monterey, Calif. "This thesis was done at the MOVES Institute."--Cover. Includes bibliographical references (p. 133-137). Also available online from the Naval Postgraduate School (NPS), Dudley Knox Library and the DTIC Online Web sites.
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An experimental study of flow about an airfoil with slotted flap and spoiler using Joukowsky profilesAllan, William D. E. January 1988 (has links)
An experimental study has been carried out on an airfoil with slotted flap and spoiler using Joukowsky profiles. Pressure distributions
were measured as functions of angle of attack, flap deflection angle, spoiler size and inclination. The results are uncorrected for wind tunnel wall effects but the data base is available to carry out the corrections. The results will be used to compare with predictions of a theoretical model, yet to be worked out, which combines work previously done by Williams, Jandali, Parkinson and Yeung. This theory will involve the potential flow about a two-element 'near'-Joukowsky airfoil system. The secondary airfoil is a simulated slotted flap. Various size spoilers are introduced to the system at arbitrary angles of inclination using methods proposed by Parkinson and Yeung.
The experimental results are qualitatively reasonable and some interesting effects are observed. The behaviour of spoilers, when used with slotted flaps at various deflection angles, corresponds well with requirements of aircraft in approach or landing situations. Similarly, the use of slotted flaps alone provides the high lift at low angle of attack which is beneficial to aircraft taking off. Some recommendations are proposed for further testing with this equipment. / Applied Science, Faculty of / Mechanical Engineering, Department of / Graduate
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