Y 3.N 21/5:6/1967
|
A comparison of wing loads measured in flight on a fighter-type airplane by strain-gage and pressure-distribution methods / |
1 |
Y 3.N 21/5:6/1968
|
Flight tests of the hydrodynamic characteristics of a Japanese "Emily" flying boat / |
1 |
Y 3.N 21/5:6/1969
|
Comparative drag measurements at transonic speeds of rectangular and sweptback NACA 65-009 airfoils mounted on a freely falling body / |
1 |
Y 3.N 21/5:6/1970
|
Methods of designing cascade blades with prescribed velocity distributions in compressible potential flows / |
1 |
Y 3.N 21/5:6/1971
|
Plastic buckling of extruded composite sections in compression / |
1 |
Y 3.N 21/5:6/1972
|
Critical shear stress of a curved rectangular panel with a central stiffener / |
1 |
Y 3.N 21/5:6/1973
|
Theoretical spanwise lift distributions of low-aspect-ratio wings at speeds below and above the speed of sound / |
1 |
Y 3.N 21/5:6/1974
|
Effect of open circular holes on tensile strength and elongation of sheet specimens of some aluminum alloys / |
1 |
Y 3.N 21/5:6/1975
|
Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds / |
1 |
Y 3.N 21/5:6/1976
|
Summary of information relating to gust loads on airplanes / |
1 |
Y 3.N 21/5:6/1977
|
Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speeds / |
1 |
Y 3.N 21/5:6/1978
|
Data on the compressive strength of 75S-T6 aluminum-alloy flat panels having small, thin, widely spaced, longitudinal extruded Z-section stiffeners / |
1 |
Y 3.N 21/5:6/1979
|
A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds / |
1 |
Y 3.N 21/5:6/1980
|
Effect of forebody warp and increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio / |
1 |
Y 3.N 21/5:6/1981
|
Critical stress of ring-stiffened cylinders in torsion / |
1 |
Y 3.N 21/5:6/1982
|
An introduction to the physical aspects of helicopter stability / |
1 |
Y 3.N 21/5:6/1983
|
Longitudinal flying qualities of several single-rotor helicopters in forward flight / |
1 |
Y 3.N 21/5:6/1984
|
A semiempirical method for estimating the rolling moment due to yawing of airplanes / |
1 |
Y 3.N 21/5:6/1985
|
Elastic buckling of outstanding flanges clamped at one edge and reinforced by bulbs at other edge / |
1 |
Y 3.N 21/5:6/1986
|
Stability of Alclad plates / |
1 |