Reference manual · Krispin Technologies Archive — https://krispintech.com
14 14 ntrs.nasa.gov
Contents
- Summary of Rocket-Model Tests at Zero Lift of the Northrop MX-775B Missile Configuration from Mach Numbers of 0.9 to 1.8
- Summary of Section Data on Trailing-Edge High-Lift Devices
- NACA Conference on Aerodynamic Problems of Transonic Airplane Design
- Summary of section data on trailing-edge high-lift devices
- NACA Conference on Aerodynamic Problems of Transonic Airplane Design
- Vortex Flow Aerodynamics, volume 1
- The NACA variable-density wind tunnel
- NACA Report 824 Summary of Airfoil Data
- Application of Circulation Control Technology to Airframe Noise Reduction
- Experimental Studies of Low-Pressure Turbine Flows and Flow Control
- NASA Hybrid Thermally Efficient Core (HyTEC) Phase 2 Q3’GFY25 to Q2’GFY26 Unlimited Rights Annual Report for CLIN 1 and
- Some applications of the quasi vortex-lattice method in steady and unsteady aerodynamics
- Extended applications of the vortex lattice method
- CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
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