Search U.S. government technical reports digitized or harvested by TRAIL.
Aerodynamic Research on Fuselages with Rectangular Cross Section
NACA Conference on High-Speed Aerodynamics
The Turbulent Boundary Layer on a Rough Curvilinear Surface
Statistical Study of Turbulence: Spectral Functions and Correlation Coefficients
Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04
Experimental techniques for predicting store motions during release or ejection
Some Research on the Lift and Stability of Wing-Body Combinations
Boundary-Layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6