IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more. Airfoil section used on Langley ...

A discussion is given of the ongoing research related to laminar flow airfoils, nacelles, and wings where the laminar flow is maintained by a favorable pressure gradient, surface suction or a ...

An experimental study of the effects of trailing edge cracks and turbulent inflow will inform future models employed to ...

As the angle of attack is increased on a high-performance airfoil, a small amount of separation occurs near the leading edge. This separation causes the boundary layer to transition from laminar to ...

Testing components of supersonic aircraft in flight can be problematic, and the refined wing design of Aerion’s developmental supersonic business jet (SSBJ) is a case in point. The 40-inch by 80-inch ...

The small wind tunnel with a 16-by-16 inch test section is a low speed, open return tunnel, as shown in Figure 1. It is mainly used for airfoil section tests and teaching. he velocity is up to 50 m/s.

SAE Transactions, Vol. 116, Section 1: JOURNAL OF AEROSPACE (2007), pp. 560-575 (16 pages) This paper presents the results of a study designed to determine the level of fidelity required to accurately ...