High speed flows inside cavities are encountered in many aerospace applications including
weapon bays of combat aircraft as well as landing gear. The flow field inside these cavities …

Aeroacoustic feedback mechanisms in rectangular cavities are strongly dependent on
length-to-depth ratio and free stream velocity. The capability to predict the effects of these …

This paper presents an investigation of the flow physics and control of cavity flow oscillations
using a three-dimensional (3-D) array of steady jets located near the cavity leading edge …

Jet injection into a supersonic crossflow is a classical fluid dynamics problem with many
engineering applications. Several experimental and numerical studies have been taken up …

Experiments were performed to understand the complex fluid-structure interactions that
occur during aircraft internal store carriage. A cylindrical store was installed in a rectangular …

Motivated by the successful application of active control using segmented spanwise
blowing, this work investigates passive flow control for a rectangular cavity in supersonic …

Two flow control methods, namely, the microjet array (MJA) and the conventional shock
wave generator (SWG), were employed to enhance the chemical reaction in a strut-based …

The flow over an aircraft bay is often represented using a rectangular cavity; however, this
simplification neglects many features of actual flight geometry that could affect the unsteady …

A novel actuator concept is evaluated in a series of active flow control experiments on a
resonant high-speed cavity flow. The actuator generates pulsed supersonic microjets by …

Numerical investigations of the leading-edge sawtooth spoiler and slanted aft wall were
performed to explore the mechanisms of the suppression of pressure fluctuations in an open …