Electrical engineering

Conceptual design

Physics

Architecture

Sociology

Aerospace engineering

Mathematics

Social science

Propulsion

Statistics

Fuselage

Engineering

Visual arts

Rotor (electric)

Systems engineering

Component (thermodynamics)

Multidisciplinary approach

Set (abstract data type)

Fidelity

Programming language

Multidisciplinary design optimization

Computer science

Flexibility (engineering)

Airplane

Mechanical engineering

Thermodynamics

The theoretical basis and architecture of the conceptual design tool NDARC (NASA Design and Analysis of Rotorcraft) are described. The principal tasks of NDARC are to design (or size) a rotorcraft to satisfy specified design conditions and missions, and then analyze the performance of the aircraft for a set of off-design missions and point operating conditions. The aircraft consists of a set of components, including fuselage, rotors, wings, tails, and propulsion. For each component, attributes such as performance, drag, and weight can be calculated. The aircraft attributes are obtained from the sum of the component attributes. NDARC provides a capability to model general rotorcraft configurations, and estimate the performance and attributes of advanced rotor concepts. The software has been implemented with low-fidelity models, typical of the conceptual design environment. Incorporation of higher-fidelity models will be possible, as the architecture of the code accommodates configuration flexibility, a hierarchy of models, and ultimately multidisciplinary design, analysis and optimization.

NDARC-NASA Design and Analysis of Rotorcraft Theoretical Basis and Architecture