Donald C. Howe

发表

Impact of Engine Cycle Selection on Propulsion System Integration and Vehicle Performance for a Quiet Supersonic Aircraft

Timothy R. Conners, Donald C. Howe, John R. Whurr, 2005 .

Improved Sonic Boom Minimization with Extendable Nose Spike

Donald C. Howe, D. Howe, 2005 .

Near Field Acoustic Test on a Low Boom Configuration in Langley's 4 x 4 Wind Tunnel (Invited)

Donald C. Howe, Linda S. Bangert, Kenrick Waithe, 2011 .

CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet

Donald C. Howe, Timothy R. Conners, Stefanie M. Hirt, 2008 .

Experimental Sonic Boom Measurements on a Mach 1.6 Cruise Low-Boom Configuration

Donald C. Howe, Linda S. Bangert, Kenrick Waithe, 2012 .

Improved Sonic Boom Scaling Algorithm

Donald C. Howe, Preston A. Henne, 2006 .

A Method for Reducing Sonic Boom Strength by Tailoring the Shape of the Propulsive Streamtube

Donald C. Howe, Timothy R. Conners, Preston A. Henne, 2013 .

Supersonic Inlet Shaping for Dramatic Reductions in Drag and Sonic Boom Strength

Donald C. Howe, Timothy R. Conners, D. Howe, 2006 .

Quiet Spike Near Field Flight Test Pressure Measurements with CFD Comparisons

Donald C. Howe, Edward A. Haering, Kenrick Waithe, 2008 .

Wind Tunnel Testing of an Axisymmetric Isentropic Relaxed External Compression Inlet at Mach 1.97 Design Speed

Donald C. Howe, Timothy R. Conners, Stefanie M. Hirt, 2007 .