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  2. Aerodynamic force - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_force

    The aerodynamic force is the resultant vector from adding the lift vector, perpendicular to the flow direction, and the drag vector, parallel to the flow direction. Forces on an aerofoil . In fluid mechanics , an aerodynamic force is a force exerted on a body by the air (or other gas ) in which the body is immersed, and is due to the relative ...

  3. United States Air Force Stability and Control Digital DATCOM

    en.wikipedia.org/wiki/United_States_Air_Force...

    In February 1976, work commenced to automate the methods contained in the USAF Stability and Control DATCOM, specifically those contained in sections 4, 5, 6 and 7.The work was performed by the McDonnell Douglas Corporation under contract with the United States Air Force in conjunction with engineers at the Air Force Flight Dynamics Laboratory in Wright-Patterson Air Force Base.

  4. NAVBLUE - Wikipedia

    en.wikipedia.org/wiki/NAVBLUE

    NAVBLUE, an amalgamation of Navtech, Airbus LUCEM and Airbus ProSky, is Airbus’ flight operations software subsidiary. [1] [2] They provide products which include software for flight planning, aircraft performance, flight data analysis, aeronautical charts, crew planning, [3] [4] electronic flight bag and navigational data.

  5. Tomark Viper SD4 - Wikipedia

    en.wikipedia.org/wiki/Tomark_Viper_SD4

    The first two production aircraft appeared at AERO Friedrichshafen in April 2007. AERO 2009 saw the first example of the Ultralight version and the announcement of the LSA variant [1] It was originally aimed at French flying clubs [1] but is now being marketed in the USA following certification in October 2010.

  6. Systems Tool Kit - Wikipedia

    en.wikipedia.org/wiki/Systems_Tool_Kit

    Systems Tool Kit (formerly Satellite Tool Kit), often referred to by its initials STK, is a multi-physics software application from Analytical Graphics, Inc. (an Ansys company) that enables engineers and scientists to perform complex analyses of ground, sea, air, and space platforms, and to share results in one integrated environment. [1]

  7. Aerodynamic center - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_center

    The aerodynamic center is the point at which the pitching moment coefficient for the airfoil does not vary with lift coefficient (i.e. angle of attack), making analysis simpler. [ 1 ] d C m d C L = 0 {\displaystyle {dC_{m} \over dC_{L}}=0} where C L {\displaystyle C_{L}} is the aircraft lift coefficient .

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