| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/3217 | The influence of wheel spin-up on landing-gear impact / | 1 |
| Y 3.N 21/5:6/3218 | Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8 / | 1 |
| Y 3.N 21/5:6/3219 | Viscosity corrections to cone probes in rarefied supersonic flow at a nominal Mach number of 4 / | 1 |
| Y 3.N 21/5:6/3220 | Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section / | 2 |
| Y 3.N 21/5:6/3221 | Study of the subsonic forces and moments on an inclined plane of infinite span / | 1 |
| Y 3.N 21/5:6/3222 | Measurement of heat transfer in the turbulent boundary layer on a flat plate in supersonic flow and comparison with skin-friction results / | 1 |
| Y 3.N 21/5:6/3223 | An analysis of shock-wave cancellation and reflection for porous walls which obey an exponential mass-flow pressure-difference relation / | 1 |
| Y 3.N 21/5:6/3224 | Theoretical investigation of the effects upon lift of a gap between wing and body of a slender wing-body combination / | 1 |
| Y 3.N 21/5:6/3225 | An experimental study of the lift and pressure distribution on a double-wedge profile at Mach numbers near shock attachment / | 1 |
| Y 3.N 21/5:6/3226 | Some possibilities of using gas mixtures other than air in aerodynamic research / | 1 |
| Y 3.N 21/5:6/3227 | Application of two-dimensional vortex theory to the prediction of flow fields behind wings of wing-body combinations at subsonic and supersonic speeds / | 1 |
| Y 3.N 21/5:6/3228 |
Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees / Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° / |
2 |
| Y 3.N 21/5:6/3229 | The small-disturbance method for flow of a compressible fluid with velocity potential and stream function as independent variables / | 1 |
| Y 3.N 21/5:6/3230 | Investigation of distributed surface roughness on a body of revolution at a Mach number of 1.61 / | 1 |
| Y 3.N 21/5:6/3231 | Bending tests on box beams having solid- and open-construction webs / | 1 |
| Y 3.N 21/5:6/3232 | An analysis of the stability and ultimate bending strength of multiweb beams with formed-channel webs / | 1 |
| Y 3.N 21/5:6/3233 | A review of planing theory and experiment with a theoretical study of pure-planing lift of rectangular flat plates / | 1 |
| Y 3.N 21/5:6/3234 | Reduction of helicopter parasite drag / | 1 |
| Y 3.N 21/5:6/3235 | Low-speed yawed-rolling and some other elastic characteristics of two 56-inch-diameter, 24-ply-rating aircraft tires / | 1 |
| Y 3.N 21/5:6/3236 | Wind-tunnel studies of the performance of multirotor configurations / | 1 |
