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Showing 1 to 4 of 4 for “"USAF DatCom"”.

  1. Evaluation and Flight Assessment of a Scale Glider

    … was also completed and compared using SURFACES, USAF Datcom, and MIT AVL software. The glide slope estimate and stability and control derivatives obtained from flight test data showed considerable range and uncertainty. Potential sources of noisy test data and model flaws are discussed in detail. …

    embry-riddle Repository record for Evaluation and Flight Assessment of a Scale Glider (opens in a new tab)

  2. Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES

    … the scale from 0.6 meters to 1.2 meters. Using USAF DatCom methods, a spreadsheet program for predicting the dynamic stability and handling qualities of small UAVs was created for use in the design stage of new small UAV concept development. This program was verified by inputting data for a …

    byu Repository record for Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES (opens in a new tab)

  3. The enhancement of a flight simulator system with teaching and research applications

    … longitudinal stability of an aircraft using the USAF DATCOM method as a basis. This program demonstrates all the steps in the solution including the use of all necessary graphical data. Following an introduction outlining the history and objectives of this work, chapter two details the …

    concordia Repository record for The enhancement of a flight simulator system with teaching and research applications (opens in a new tab)

  4. Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei)

    … on methods available in Jan Roskam textbooks and USAF DATCOM. The model used Thrust and Specific Fuel Consumption data presented in Jenkinson, L.R., Simpkin, P., and Rhodes, D., "Civil Jet Aircraft Design," and detailed aircraft geometry properties given in Jane's All the World Aircraft as well as …

    unsw Repository record for Range and endurance modelling of a multi-engine aircraft with one engine inoperative (oei) (opens in a new tab)