A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

The development of the boundary layer and the interaction of the boundary layer with the
outer “inviscid” flow field, exacerbated at high speed by the occurrence of shock waves …

Ultra Efficient Engine Technology (UEET) program in late 1999 [1–3]. This program had
several elements, one of which was to explore the feasibility of the blended-wing-body …

This paper presents a preliminary design study aimed to verify the feasibility of an adaptive
wing for a small unmanned aircraft (UAV), which is entirely actuated by shape memory alloy …

The effectiveness of several active and passive devices to control flow in an adverse
pressure gradient with secondary flows present was evaluated in the 15 Inch Low Speed …

The effect of passive flow control using an oscillating micro-cylinder near the leading edge of
a stalled airfoil (S809) at a Reynolds number of 1× 10 6 is numerically investigated. A …

Boundary layer ingestion (BLI) is explored as a means to improve overall system
performance for a Blended Wing Body configuration. The benefits of BLI for vehicle system …

Shock-induced separation is a common phenomenon in aero-space transportation
applications which can result in strong detrimental effects. A promising method of passive …

Aiming at the problem that the exciting force induced by the propeller is excessive and the
hull vibration noise exceeds certain limits for a certain surface ship, a type of triangular …

Toward Understanding and Optimizing Separation Control Using Microjets Page 1 Toward
Understanding and Optimizing Separation Control Using Microjets Vikas Kumar ∗ and Farrukh …