Sadraey, 2012 - Google Patents
Wing designSadraey, 2012
View PDF- Document ID
- 14395223739970177607
- Author
- Sadraey M
- Publication year
- Publication venue
- Aircraft Design: A Systems Engineering Approach
External Links
Snippet
In chapter 4, aircraft preliminary design–the second step in design process–was introduced. Three parameters were determined during preliminary design, namely: aircraft maximum takeoff weight (WTO); engine power (P), or engine thrust (T); and wing reference area (Sref) …
- 238000009826 distribution 0 abstract description 65
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically
- B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
- B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/008—Rotors tracking or balancing devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Antcliff et al. | Baseline assumptions and future research areas for urban air mobility vehicles | |
Seitz et al. | The DLR project LamAiR: design of a NLF forward swept wing for short and medium range transport application | |
Hitchens | The encyclopedia of aerodynamics | |
Sadraey | Wing design | |
Scholz | Empennage sizing with the tail volume complemented with a method for dorsal fin layout | |
Minardo | The tandem wing: theory, experiments and practical realisations | |
Yeo et al. | Aeromechanics analysis of a heavy lift slowed-rotor compound helicopter | |
Spacht | The forward swept wing-a unique design challenge | |
Leishman et al. | Challenges in the Aerodynamic Optimization of High‐Efficiency Proprotors | |
Zuhair et al. | Trailing edge geometry effect on the aerodynamics of low-speed BWB aerial vehicles | |
De Resende | The evolution of the aerodynamic design tools and transport aircraft wings at Embraer | |
Ibrahim | Selecting principal parameters of baseline design configuration for twin turboprop transport aircraft | |
Badis | Subsonic aircraft wing conceptual design synthesis and analysis | |
ALGÜL | WİNG DESİGN AND AERODYNAMİC ANALYSİS OF VLA AIRCRAFT | |
Stroub | Introduction of the M-85 high-speed rotorcraft concept | |
Ibrahim | AIRCRAFT DESIGN REPORT | |
Mulyanto et al. | Conceptual design of blended wing body business jet aircraft | |
SHARDA et al. | DESIGN OF E-VTOL AIRCRAFT WITH TILT-WINGS | |
Eraslan | A training sailplane design | |
Kanistras et al. | Aircraft performance and design | |
NAYUDU | DESIGN OF AMPHIBIAN AIRCFRAFT WITH VTOL MECHANISM | |
DHANIYALAKSHMI et al. | DESIGN OF BUSINESS JET WITH MORPHING WINGS | |
JOSEPH | DESIGN OF CARGO AIRCRAFT AEB336 DESIGN PROJECT-1 REPORT | |
BHARDWAJ | DESIGN OF CARGO AIRCRAFT AEB336 DESIGN PROJECT-1 REPORT | |
KARTHIK | DESIGN OF CARGO AIRCRAFT AEB336 DESIGN PROJECT-1 REPORT |