Work

Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability

Year: 1991

Type: article

Abstract: An investigation was conducted in the static test facility of the Langley 16 Foot Transonic Tunnel in order to determine the internal performance characteristics of a multiaxis thrust vectoring axisymmetric nozzle. Thrust vectoring for this nozzle was achieved by deflection of only the divergent section of this nozzle. The effects of nozzle power setting and divergent flap length were studied at nozzle deflection angles of 0 to 30 at nozzle pressure ratios up to 8.0.

Source: University of Michigan Library Repository

Authors: George T. Carson, F. J. Capone

Institution: Langley Research Center

Language: English

Topic: Rocket and propulsion systems research

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W303400937

FWCI: 7.275

Cites:

Cited by: 22

Related to: 10