NASA Technical Reports Server (NTRS) : The pdf

NASA Technical Reports Server (NTRS) : The_bookcover

NASA Technical Reports Server (NTRS) : The

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The overall goal was to investigate and exploit the advantages of using remotely powered vehicles (RPV’s) for in-flight data collection at low Reynold’s numbers. The data to be collected is on actual flight loads for any type of rectangular or tapered airfoil section, including vertical and horizontal stabilizers. The data will be on a test specimen using a force-balance system which is located forward of the aircraft to insure an undisturbed air flow over the test section. The collected data of the lift, drag and moment of the test specimen is to be radioed to a grand receiver, thus providing real-time data acquisition. The design of the mission profile and the selection of the instrumentation to satisfy aerodynamic requirements are studied and tested. A half-size demonstrator was constructed and flown to test the flight worthiness of the system

  • Creator/s: NASA Technical Reports Server (NTRS
  • Date: 1/1/1989
  • Year: 1989
  • Book Topics/Themes: NASA Technical Reports Server (NTRS), AERODYNAMIC INTERFERENCE, AERODYNAMIC LOADS, AIR FLOW, AIRFOIL PROFILES, DATA ACQUISITION, DATA COLLECTION PLATFORMS, FLIGHT STABILITY TESTS, FORCE DISTRIBUTION, REMOTELY PILOTED VEHICLES, STABILIZERS (FLUID DYNAMICS), AERODYNAMIC DRAG, AUTOMATIC CONTROL, BALANCE, LOW REYNOLDS NUMBER, PROVING, REAL TIME OPERATION, TEST CHAMBERS, STABILITY DERIVATIVES, Bryan, Kevin, Soutar, John, Witty, Peter, Mediate, Bruno, Quast, Thomas, Combs, Dan, Schubert, Martin, Condron, David, Taylor, Scott, Garino, ED

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