1. Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft;Larson
2. Use of nose cap and fuselage pressure orifices for determination of air data for space shuttle orbiter below supersonic speed;Larson
3. Comparison of predicted and experimental real – gas pressure distributions on space shuttle orbiter nose for shuttle entry air data system;Shin
4. Shuttle Entry Air Data System (SEADS)-Flight Verification of an Advanced Airdata System Concept;Siemers
5. Subsonic Tests of an All-Flush-Pressure-Orifice Airdata System;Larson,1981