Recent developments in wind-tunnel testing techniques at transonic and supersonic speeds

This publication has 9 references indexed in Scilit:

• PRESSURE FLUCTUATIONS RESULTING FROM AN ALTERNATING FLOW SEPARATION AND ATTACHMENT AT TRANSONIC SPEEDS
  Published by Defense Technical Information Center (DTIC) ,1963
• BASE HEATING ON A MULTIPLE PROPULSION NOZZLE MISSILE
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1963
• QUASI-STEADY ASPECTS OF THE ADJUSTMENT OF SEPARATED FLOW REGIONS TO TRANSIENT EXTERNAL FLOWS
  AIAA Journal, 1963
• The Design and Dynamic Calibration of a Pressure Transducer System for Unsteady Pressure Measurements.
  Published by Defense Technical Information Center (DTIC) ,1963
• Tecnical Notes
  ARS Journal, 1961
• A SUMMARY OF PERFORATED WALL WIND TUNNEL STUDIES AT THE ARNOLD ENGINEERING DEVELOPMENT CENTER
  Published by Defense Technical Information Center (DTIC) ,1960
• Some Studies of the Flow Pattern at the Base of Missiles with Rocket Exhaust Jets
  Published by Defense Technical Information Center (DTIC) ,1960
• Reflection of a Wave at an Interface of Supersonic Flows and Wave Patterns in a Supersonic Compound Jet
  Journal of the Physics Society Japan, 1952
• Axial Magnetic Suspensions
  Review of Scientific Instruments, 1937