Norman S. Land

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The Effect of Afterbody Length of the Hydrodynamic Stability of a Dynamic Model of a Flying Boat: Langley Tank Model 134

Norman S. Land, 1945 .

Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat

Norman S. Land, Roland E. Olson, 1949 .

Acceleration Measurements During Landing in Rough Water of a 1/7-Scale Dynamic Model of Grumman XJR2F-1 Amphibian - Langley Tank Model 212, TED No. NACA 2378

Norman S. Land, Howard Zeck, 1947 .

Methods Used in the NACA Tank for the Investigation of the Longitudinal-Stability Characteristics of Models of Flying Boats

Norman S. Land, Roland E. Olson, 1943 .

Tank Tests of a 1/7-Size Dynamic Model of the Grumman XJR2F-1 Amphibian to Determine the Effect of Slotted- and Split-Type Flaps on Take-Off Stability - NACA Model 212, TED No. NACA 2378

Norman S. Land, Howard Zeck, 1947 .

An Investigation of Hydrofoils in the NACA Tank. 1 - Effect of Dihedral and Depth of Submersion

Norman S. Land, James M. Benson, 1942 .

Tank Tests of an Alternate Hull Form for the Consolidated Vultee Pb2y-3 Airplane

Norman S. Land, Jack Posner, 2013 .

Tank Tests of a 1/7-Size Powered Dynamic Model of the Grumman XJR2F-1 Amphibian: Spray Characteristics, Take-Off and Landing Stability in Smooth Water - Langley Tank Model 212, TED No. NACA 2378

Norman S. Land, Howrad Zeck, 1946 .

Full-Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425-Scale XP5M-1 Hull Bottom: TED No. NACA DE325

Norman S. Land, John M. Elliott, Kenneth W. Christopher, 1949 .

Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane. TED No. NACA DE 357

Norman S. Land, Charles A. Pelz, 1952 .

An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-Tail

Norman S. Land, Annie G. Fox, 1961 .