Incoming Resources
- Predictions of supersonic jet mixing and shock-associated noise compared with measured far-field data, Milo D. Dahl
- An experimental evaluation of the performance of two combination pitot pressure probes, David J. Arend and John D. Saunders ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
- Large-scale Advanced Propfan (LAP) performance, acoustic and weight estimation, January, 1984, D. Parzych, [S. Cohen, A. Shenkman]
- Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79, Bianca Trujillo Anderson and Robert R. Meyer, Jr
- Slot nozzle effects for reduced sonic boom on a generic supersonic wing section, Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010
- Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825, Bianca Trujillo Anderson and Robert R. Meyer, Jr
- Equivalent longitudinal area distributions of the B-58 and XB-70-1 airplanes for use in wave drag and sonic boom calculations, Ana F. Tinetti [and others]
- Mach 5 inlet CFD and experimental results, Lois J. Weir, and D. R. Reddy, and George D. Rupp
- Local flow conditions for proplusion experiments on the F-15B Propulsion Flight Test Fixture, Michael J. Vachon, Timothy R. Moes, Stephen Corda