Call Number (LC) Title Results
Y 3.N 21/5:6/699 Tests of an N.A.C.A. 23012 airfoil with a slotted deflector flap /
Tests of N. A. C. A. 23012 airfoil with slotted deflector flap. 		3
Y 3.N 21/5:6/700 Theory of automatic control of airplanes /
Theory of automatic control of airplanes. 		3
Y 3.N 21/5:6/701 Intermittent-flow coefficients of a poppet valve /
Intermittent-flow coefficients of a poppet valve. 		3
Y 3.N 21/5:6/702 Wind-tunnel tests of several forms of fixed wing slot in combination with a slotted flap on an N.A.C.A. 23012 airfoil /
Wind℗--tunnel tests of several forms of fixed wing slot in combination with slotted flap on N. A. C. A. 23012 airfoil. 		3
Y 3.N 21/5:6/703 Wind-tunnel investigation of effect of yaw on lateral-stability characteristics.
Wind℗--tunnel investigation of effect of yaw on lateral-stability characteristics : 1, Four N. A. C. A. 23012 wings of various plan forms with and without dihedral.
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. : 1 - Four N.A.C.A. 23012 wings of various plan forms with and without dihedral / 		3
Y 3.N 21/5:6/704 Some notes on the numerical solution of shear-lag and mathematically related problems /
Some notes on the numerical solution of shear-lag and mathematically related problems. 		3
Y 3.N 21/5:6/705 Wind-tunnel investigation of ground effect on wings with flaps /
Wind-tunnel investigation of ground effect on wings with flaps. 		3
Y 3.N 21/5:6/706 An experimental investigation of the normal acceleration of an airplane model in a gust /
An Experimental investigation of the normal acceleration of an airplane model in a gust /
An experimental investigation of the normal acceleration of an airplane model in a gust. 		3
Y 3.N 21/5:6/707 Compression-ignition engine performance with undoped and doped fuel oils and alcohol mixtures /
Compression-ignition engine performance with undoped and doped fuel oils and alcohol mixtures. 		3
Y 3.N 21/5:6/708 A simplified method for the calculation of airfoil pressure distribution /
A Simplified method for the calculation of airfoil pressure distribution /
A simplified method for the calculation of airfoil pressure distribution. 		3
Y 3.N 21/5:6/709 A semi-graphical method for analyzing strains measured on three or four gage lines intersecting at 45° /
A Semi-graphical method for analyzing strains measured on three or four gage lines intersecting at 45 degrees /
A semi℗--graphical method for analyzing strains measured on three or four gage lines intersecting at 45℗ʻ 		3
Y 3.N 21/5:6/710 A comparison of ignition characteristics of diesel fuels as determined in engines and in a constant-volume bomb /
A Comparison of ignition characteristics of diesel fuels as determined in engines and in a constant-volume bomb /
A comparison of ignition characteristics of diesel fuels as determined in engines and in a constant℗--volume bomb. 		3
Y 3.N 21/5:6/711 An approximate spin design criterion for monoplanes /
An Approximate spin design criterion for monoplanes /
An approximate spin design criterion for monoplanes. 		3
Y 3.N 21/5:6/712 A preliminary study of the prevention of ice on aircraft by the use of engine-exhaust heat /
A Preliminary study of the prevention of ice on aircraft by the use of engine-exhaust heat /
A preliminary study of the prevention of ice on aircraft by the use of engine℗--exhaust heat. 		3
Y 3.N 21/5:6/713 A comparison of several tapered wings designed to avoid tip stalling /
A Comparison of several tapered wings designed to avoid tip stalling /
A comparison of several tapered wings designed to avoid tip stalling. 		3
Y 3.N 21/5:6/714 Flight tests of retractable ailerons on a highly tapered wing /
Flight tests of retractable ailerons on a highly tapered wing. 		3
Y 3.N 21/5:6/715 Wind-tunnel investigation of an N.A.C.A. 23012 airfoil with two arrangements of a wide-chord slotted flap /
Wind-tunnel investigation of N. A. C. A. 23012 airfoil with two arrangements of a wide-chord slotted flap. 		3
Y 3.N 21/5:6/716 Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise : N.A.C.A. models 57-A, 57-B, and 57-C /
Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise. : N.A.C.A. models 57-A, 57-B, and 57-C /
Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise, N. A. C. A. models 57-A, 57-B, and 57-C. 		3
Y 3.N 21/5:6/717 A method of estimating the critical buckling load for structural members /
A Method of estimating the critical buckling load for structural members /
A method of estimating the critical buckling load for structural members. 		3
Y 3.N 21/5:6/718 Resistance of transparent plastics to impact /
Resistance of transparent plastics to impact. 		3