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11	The effects of nonstationary aerodynamics on the rigid-body dynamic stability of an airplane Statler, Irving C. January 1956 (has links) Thesis--California Institute of Technology. / Includes bibliographical references.
12	The effects of nonstationary aerodynamics on the rigid-body dynamic stability of an airplane Statler, Irving C. January 1956 (has links) Thesis--California Institute of Technology. / Includes bibliographical references.
13	Adaptive nonlinear flight control Rysdyk, Rolf T. 12 1900 (has links) No description available. Airplanes Control systems Stability of airplanes Aerodynamics
14	Longitudinal handling characteristics of a tailless gull-wing aircraft Agenbag, Daniël Sarel. January 2008 (has links) Thesis (MEng (Mechanical engineering))-University of Pretoria, 2008. / Includes bibliographical references.
15	Development of a variable stability flight simulation facility re-engineering of flight control loading and motion systems / Scamps, Alexander. January 2003 (has links) Thesis (M.E. (Res.))--University of Sydney, 2003. / Title from title screen (viewed Apr. 28, 2008). Submitted in fulfilment of the requirements for the degree of Master of Engineering (Research) to the School of Aerospace, Mechanical and Mechatronic Engineering. Includes bibliography. Also available in print form.
16	Dynamic stability and handling qualities of small unmanned-aerial-vehicles / Foster, Tyler M. January 2005 (has links) (PDF) Thesis (M.S.)--Brigham Young University. Dept. of Mechanical Engineering, 2005. / Includes bibliographical references (p. 97-98).
17	Development of deployable wings for small unmanned aerial vehicles using compliant mechanisms / Landon, Steven D., January 2007 (has links) (PDF) Thesis (M.S.)--Brigham Young University. Dept. of Mechanical Engineering, 2007. / Includes bibliographical references (p. 113-116).
18	System identification and parameter estimation of the Piper PA32-301 Saratoga Kelly, Catherine Anne, January 2006 (has links) (PDF) Thesis (M.S.) -- University of Tennessee, Knoxville, 2006. / Title from title page screen (viewed on Feb. 5, 2007). Thesis advisor: Ralph D. Kimberlin. Vita. Includes bibliographical references.
19	A Method for Approximating the Distributed Loads of an Airplane by Sets of Point Loads Austin, Charles Wayne January 1957 (has links) This paper gives the derivation of a method for determining the forces to be applied to these points which will simulate the load distributed over all the airplane. distributed loads airplane point loads Airplanes -- Weight. Stability of airplanes.
20	Analysis of various forced oscillation techniques for obtaining dynamic stability derivatives Ko, Joon Soo January 1982 (has links) Existing subsonic wind tunnel methods for obtaining dynamic stability derivatives for aircrafts at high angle of attack are described. From the general equations of motion of an aircraft in space, the perturbation equations of motion are derived for applying to a wind tunnel aircraft model. Data Reduction and test procedures for important dynamic tests are evolved systematically from the restrained perturbed equations of motion. Emphasis is given to the typical single degree of freedom apparatuses and associated data reduction for routine measurement of dynamic stability derivatives due to pitching, rolling and yawing of the model. The translational and snaking motion apparatuses from which the derivatives, α, β, and p, q, r are measured separately, are also presented. Finally, for the purpose of increasing the capabilities of the Virginia Tech dynamic test systems, a single degree of freedom forced oscillatory rig, which gives the exact sinusoidal displacement of the model and also adjustable to the existing curved and rolling flow facilities, is described with its data acquisition/reduction. / Master of Science LD5655.V855 1982.K672 Wind tunnels Aerodynamics Stability of airplanes

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