1. Evaluation of acoustic testing techniques for spacecraft systems;Cockburn;Wyle Laboratories Research Staff WR,1971
2. Wind tunnel investigation of the effects of Reynolds number and model size on the steady and fluctuating pressures experienced by conecylinder missile configurations at transonic speeds;Robertson;AEDC-TR-66-266, Arnold Engineering Development Center, Air Force Systems Command, Arnold Air Force Station, Tennessee,1967
3. Atlas-Centaur AC-11 flight performance for Surveyor IV;Center;NASA TMX-1768,1969
4. Surface pressure fluctuations associated with aerodynamic noise;Coe,1969
5. Prediction of boundary layer pressure fluctuations;Lowson;Wyle Laboratories Research Staff WR,1967