Add to ORKGThesis (B.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1954.MIT copy bound with: An investigation and comparison of the subsonic aerodynamic characteristics of the swept and crescent wing configurations / William Strike & George Perrone [1954]Includes bibliographical references (leaf 38).by Milton Toorans.B.S
Initially conceptualised by Benad in 2015 as a highly swept flying wing aircraft to replace the A350...
This research develops and analyses a general aviation plane. A preliminary representation of the ev...
Thesis (B.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1953.MIT cop...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
The main topic of this mechanical engineering design project is to redesign the landing gear of the...
The aircraft under consideration in the following text is a swing wing, 50,000 lb. (maximum weight)...
Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
Thesis (B.S.) Massachusetts Institute of Technology. Dept. of Mechanical Engineering, 1947.Bibliogra...
This research develops and analyses a general aviation plane. A preliminary representation of the ev...
This report presents an investigation of the design and construction of various types of landing gea...
Initially conceptualised by Benad in 2015 as a highly swept flying wing aircraft to replace the A350...
This research develops and analyses a general aviation plane. A preliminary representation of the ev...
Thesis (B.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1953.MIT cop...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
The main topic of this mechanical engineering design project is to redesign the landing gear of the...
The aircraft under consideration in the following text is a swing wing, 50,000 lb. (maximum weight)...
Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-d...
Thesis (B.S.) Massachusetts Institute of Technology. Dept. of Mechanical Engineering, 1947.Bibliogra...
This research develops and analyses a general aviation plane. A preliminary representation of the ev...
This report presents an investigation of the design and construction of various types of landing gea...
Initially conceptualised by Benad in 2015 as a highly swept flying wing aircraft to replace the A350...
This research develops and analyses a general aviation plane. A preliminary representation of the ev...
Thesis (B.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1953.MIT cop...