Search results
Results from the WOW.Com Content Network
Indonesian Aerospace (IAe) (Indonesian: PT Dirgantara Indonesia), is an Indonesian aerospace company involved in aircraft design and the development and manufacture of civilian and military regional commuter aircraft, and a subsidiary of state-owned electronics manufacturer Len Industri [].
Location of Bawean. The incident began at 11:38 UTC+7:00 on 3 July 2003 when military-civilian radar at Ngurah Rai International Airport in Denpasar, Bali detected suspicious movement of several aircraft northwest of Bawean Island, with the altitude observed to be between 15,000 ft (4,600 m) to 35,000 ft (11,000 m) and speed of 450 kn (830 km/h).
Sultan Hasanuddin International Airport (IATA: UPG, ICAO: WAAA) is an international airport serving Makassar, South Sulawesi, Indonesia.It is located 20 km (12 mi) northeast of Makassar's city centre and is operated by PT.
Mean aerodynamic chord (MAC) is defined as: [6] = (), where y is the coordinate along the wing span and c is the chord at the coordinate y.Other terms are as for SMC. The MAC is a two-dimensional representation of the whole wing. The pressure distribution over the entire wing can be reduced to a single lift force
Angle of incidence of an airplane wing on an airplane. On fixed-wing aircraft, the angle of incidence (sometimes referred to as the mounting angle [1] or setting angle) is the angle between the chord line of the wing where the wing is mounted to the fuselage, and a reference axis along the fuselage (often the direction of minimum drag, or where applicable, the longitudinal axis).
The AgustaWestland Apache is a licence-built version of the Boeing AH-64D Apache Longbow attack helicopter for the British Army Air Corps.The first eight helicopters were built by Boeing; the remaining 59 were assembled by Westland Helicopters (later AgustaWestland) at Yeovil, Somerset in England from Boeing-supplied kits.
In larger aircraft, weight and balance is often expressed as a percentage of mean aerodynamic chord, or MAC. For example, assume the leading edge of the MAC is 62 inches aft of the datum. Therefore, the CG calculated above lies 32 inches aft of the leading edge of the MAC. If the MAC is 80 inches in length, the percentage of MAC is 32 / 80 = 40%.
For symmetrical airfoils =, so the aerodynamic center is at 25% of chord measured from the leading edge. But for cambered airfoils the aerodynamic center can be slightly less than 25% of the chord from the leading edge, which depends on the slope of the moment coefficient, . These results obtained are calculated using the thin airfoil theory so ...