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Search Results: Returned 6 Results, Displaying Titles 1 - 6
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-- Engineer's data bookc2005., ASME Press Call No: TJ 151 .M392 2005 Edition: 2nd ed. Availability:1 of 1 At Location(s)
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Source : MS 20-Victory, John F. Format : application/pdf United States Air Force AcademyDescription
The John F. Victory Collection (MS 20) was donated to the Air Force Academy by John’s wife, Marie, in 1977. The collection includes 64 archival boxes containing photographs, manuscripts, correspondence, and official reports documenting the entire history of NACA and Victory’s involvement in the agency. This collection maintains the original order in which it was received and has been divided into twelve series, outlined in the Scope and Content section of the finding aid. See Oral History file no. 210 for interviews with John F. Victory in 1962 and 1970.
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Source : SMS 703-Edwards, Wilson V. Format : application/pdf United States Air Force AcademyDescription
1939-2008; World War II; military records 201 file; Eagle Squadron Association; Eagle Squadrons; reunions; ESU Business Meetings; Eagle Squadron Memorial; Mark 16 Spitfire memorial; Royal Air Force (RAF); Spitfire aircraft; Hawker Hurricane aircraft; B-17F Flying Fortress; Bf-109G; Thunderbolt; P-51; D-Day; Prisoners of War (POW); Air Raid Precautions Department; Air Training Command; USAAF; Fourth Fighter Wing; Strategic Air Command; U.S. Military missions abroad; Colorado Aviation Hall of Fame; aviation; aerial navigation; AAF Office of Flying Safety; Headquarters Army Air Forces; Commanding General, Army Air Forces; U.S. Department of Commerce, Civil Aeronautics Administration; War Department; Clark Special Collections; Prisoners of War (POW); Stalag Luft III; Finding Aids Edwards, Wilson V.; Tilley, Reade; Caine, Phillip; Smith, "Snuffy" Don; "Cookie" United States; England; Germany; Ireland; Saudi Arabia; Pakistan
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Source : Michael L. Anderson Collection Format : application/pdf United States Air Force AcademyDescription
Journal of Guidance, Control, and Dynamics, Vol 37, No 1, pp 290-300, 2014, accessed January 08, 201 Abstract: Flapping wing micro air vehicles continue to be a growing field, with ongoing research into unsteady, low Reynolds number aerodynamics, microfabrication, and fluid–structure interaction. However, research into flapping wing control of such micro air vehicles continues to lag. Existing research uniformly consists of proposed control laws that are validated by computer simulations of quasi-steady blade-element formulas. Such simulations use numerous assumptions and cannot be trusted to fully describe the flow physics. Instead, such control laws must be validated on hardware. In earlier work, a novel control technique, biharmonic amplitude and bias modulation, was proposed and analyzed with these same quasi-steady blade-element formulas. In this work, the biharmonic amplitude and bias modulation control technique was implemented on a flapping wing prototype (4 cm wing length)
