Comparison of wind tunnel and flight testmeasurements of static aerodynamic loading of a captive store
Comparison of wind tunnel and flight testmeasurements of static aerodynamic loading of a captive store
- New search for: Dix, R.E.
- New search for: Mattasits.G.R.
- New search for: Dix, R.E.
- New search for: Mattasits.G.R.
A coordinated series of experiments was conducted in three wind tunnels and in flight to measure the static aerodynamic loading of a MK 83 store attached to the bottom center station of a triple ejector rack mounted on the left inboard pylon of an f-4 aircraft. Fundamental agreement between wind tunnel and inflight loads data was demonstrated over a range of angle of attack from -2 to 6 deg and a Mach number range from 0.6 to 0.9. Differences that were noted were thought to be attributable either to improper store-to-aircraft alignment or to poor definition of inertial loads during maneuvering flight. (DePo)
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Comparison of wind tunnel and flight testmeasurements of static aerodynamic loading of a captive store
Vergleich zwischen Windkanal- und Flugpruefung statischer, aerodynamischer Lasten verursacht durch mitgefuehrte Ausruestung
US Government Research Reports ; Jul ; 1-117
1980
117 Seiten
Report
English
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