1D Modeling of HVAC Unit Air Flow for Automatic Climate Control Simulations
1-D Model of the 4 Bed Molecular Sieve of the Carbon Dioxide Removal Assembly
2.75-In. Folding Fin Aircraft Rocket. Volume 2. Appendixes
4th Symposium on Electromagnetic Launch Technology, 12-14 April 1988, Austin, TX, USA
Ablative Thermal Response Analysis Using the Finite Element Method
Absolute Measurements of Air Shock-Layer Radiation in the T6 Aluminium Shock Tube
Accelerated Particles from Turbulent Boundary Layer
Acceptance Testing of the Cold Air Supply to Third Stage and Satellite, Launcher 6 A, Woomera
Accommodations and equipment of special cars for testing heating installations on German railroads
Accuracy of Re-Entry Flight Test Data Needed to Determine Re-Entry AERO-Thermodynamic Parameters
Achievement of Superior Cabin Comfort and Maximising Energy Efficiency Using EXV in BEVs
Acoustic Conception of an Automotive HVAC
Acoustic Investigations of HVAC Systems in Vehicle
Acoustic Optimization of HVAC Systems
Active vibration control applied to a tram HVAC unit