Airfoil Aerodynamics & Vortex Method Reference

Reference manual · Krispin Technologies Archive — https://krispintech.com

This manual assembles federal public publications on this subject into one browsable document. Each section corresponds to one source report and keeps its original citation link. It is meant as a verification entry point, not a replacement for the source.

14 sections, compiled from 14 U.S. federal government publications (ntrs.nasa.gov). The sources are works of the U.S. federal government and are in the public domain. This compilation only selects, orders and indexes them; it reproduces no copyrighted standard text and rewrites no figure.

Contents

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

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Full text, original sources and the downloadable index are on the source site: https://krispintech.com