Rahmani et al., 2022 - Google Patents
Comparison of low-and high-order CFD based estimates of forces, moments and aerodynamic coefficients with UAS flight test dataRahmani et al., 2022
- Document ID
- 14738948390488798424
- Author
- Rahmani S
- Wang Z
- Matt J
- Chao H
- Zheng C
- Publication year
- Publication venue
- AIAA AVIATION 2022 Forum
External Links
Snippet
View Video Presentation: https://doi. org/10.2514/6.2022-4065. vid The aerodynamic coefficients and stability derivatives generated by a variety of low-and-high fidelity computational simulations were compared to flight test. It was found that at zero angle of …
- 230000010006 flight 0 title abstract description 70
Classifications
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- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5095—Vehicle design, e.g. aircraft or automotive design
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/46—Fuselage
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