Wind tunnels -- Testing

Wind-tunnel evaluation of an aeroelastically conformable rotor

Lawreence R. Sutton, Richard P. White, Jr., Robert L. Marker ; prepared for Applied Technology Laboratory, U.S. Army Research and Technology Laboratories (AVRADCOM).

National Transonic Facility (NTF) prototype fan blade fatigue test

E.H. Dean, A.J. Gustafson, D.M. Saylor.

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86

Milton Lamb.

Effects of cortex flaps on the low-speed aerodynamic characteristics of an arrow wing

Long P. Yip and Daniel G. Murri.

Evaluation of pylon focusing for reduced helicopter vibration

R. Gabel and D. Reed ; prepared for Applied Technology Laboratory, U.S. Army Research and Technology Laboratories (AVRADCOM).

Wind-tunnel experiments on divergence of forward-swept wings

Rodney H. Ricketts and Robert V. Doggett, Jr.

Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6

Robert L. Calloway

Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6

Robert L. Calloway

Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6

Robert L. Calloway.

A theory for predicting boundary impedance and resonance, frequencies of slotted-wall wind tunnels, including plenum effects

Raymond L. Barger.