because sweptback wings are less curved than normal rectangular wings and the shockwaves that form at supersonic flight form on curved surfaces, the less curved surfaces on sweptback wings make the shockwave form for a shorter time increasing the mach critical number and reducing drag a lot. genius
It is called a gear tooth. There can be many types of teeth based on the gear design; such as spur, helical, straight bevel, spiral bevel, hypoid, and several others.
You might want to check out. - Industry Design(er) - Automotive design(er)
The vertical portion of the I-beam resists shear force better than a rectangular one. The "I" portion also deflects force because of its design.
A design brief is a written document for a design project developed in concert by a person representing the business need for design and the designer. The document is focused on the desired results of design - not aesthetics. Design briefs are commonly used in consulting engagements, when an independent designer or a design agency executes a design on behalf of a client. They are less common when the designer is in-house.A design brief lists all the requirements for a specific project
A atypical design would be something simple but extravagant
No way to tell. Curly vs straight doesn't matter, only the toghness of the cable and the lock does. Curly or not, the strongest design is the better design.
Supersonic flow is characterized by speeds faster than the speed of sound. It is often used in applications such as supersonic aircraft, missiles, and high-speed wind tunnels. Supersonic flow can create shock waves and high temperatures, making it challenging to control and design for.
The properties of air flow at supersonic speeds is different than for subsonic speeds. So the design of the shape of the airplane and the inlets for the engines have to be different in order for it to fly at supersonic speeds.
Richard M. Wood has written: 'The natural flow wing-design concept' -- subject(s): Aerodynamics, Supersonic, Airplanes, Design and construction, Drag (Aerodynamics), Supersonic Aerodynamics, Triangular Wings, Wings, Wings, Triangular 'Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds' -- subject(s): Aerodynamics, Supersonic, Airplanes, Supersonic Aerodynamics, Triangular Wings, Wings, Triangular 'Study of lee-side flows over conically cambered delta wings at supersonic speeds' -- subject(s): Aerodynamics, Aerodynamics, Supersonic, Delta wing airplanes, Delta wings, Supersonic Aerodynamics, Supersonics
W. B. Fallis has written: 'Design and calibration of the Institute of Aerophysics 16in. x 16 in. supersonic wind tunnel' -- subject(s): Supersonic wind tunnels 'The design and applications of a new aerodynamic range' -- subject(s): Shock tubes
I. Frank Sakata has written: 'Evaluation of structural design concepts for an arrow-wing supersonic cruise aircraft' -- subject(s): Aerodynamics, Transonic, Supersonic planes, Transonic Aerodynamics
Supersonic travel refers to traveling at speeds faster than the speed of sound in air, which is around 343 meters per second. Supersonic aircraft use powerful engines and aerodynamic design to achieve these high speeds, enabling faster travel between destinations. However, commercial supersonic travel faces challenges such as technological limitations, environmental concerns, and regulatory restrictions.
Christopher A. Lee has written: 'Design and testing of an oblique all-wing supersonic transport' -- subject(s): Transport aircraft, Wind tunnel tests, Propulsion system configurations, Oblique wings, Supersonic wind tunnels, Wind tunnel models, Aircraft design, Supersonic transports 'I, digital' -- subject(s): Family archives, Personal archives, Digitization, Digital preservation, Archival materials
W. D. Middleton has written: 'A system for aerodynamic design and analysis of supersonic aircraft'
Vapor cones are important in the study of supersonic flight because they indicate the formation of shock waves around an object moving faster than the speed of sound. These shock waves can affect the aerodynamics and performance of the aircraft, making it crucial for engineers to understand and account for them in the design of supersonic vehicles.
J. M. Pallis has written: 'Parallelization of a parabolized Navier-Stokes solver with a design optimizer' -- subject(s): Supersonic aircraft, Hypersonic flow, Aerodynamics, Supersonic flow, Aircraft design, Supersonic transports, Navier-Stokes equation
M.L Spearman has written: 'An aerodynamic assessment of various supersonic fighter airplanes based on Soviet design concepts'