A Complete Tank Test Of A Model Of A Flying Boat Hull Naca Model No 11 A PDF Download

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A Complete Tank Test of a Model of a Flying-boat Hull - N.A.C.A. Model No. 11-A

A Complete Tank Test of a Model of a Flying-boat Hull - N.A.C.A. Model No. 11-A
Author: John B. Parkinson
Publisher:
Total Pages: 612
Release: 1933
Genre: Airplanes
ISBN:

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N.A.C.A. Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which is described in N.A.C.A. Technical Note No. 464. In contrast with the longitudinal upward curvature in the planing bottom forward of the main step on Model No. 11, the planing bottom of Model No. 11-A was made as flat as practicable. Otherwise, the two models have very nearly the same form.


A Complete Tank Test of a Model of a Flying-boat Hull - N.A.C.A. Model No. 11

A Complete Tank Test of a Model of a Flying-boat Hull - N.A.C.A. Model No. 11
Author: James M. Shoemaker
Publisher:
Total Pages: 18
Release: 1933
Genre: Airplanes
ISBN:

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This note discusses the limitations of the conventional tank test of a seaplane model. The advantages of a complete test, giving the characteristics of the model at all speeds, loads, and trim angles in the useful range are pointed out.


Tank Tests of a Family of Flying-boat Hulls

Tank Tests of a Family of Flying-boat Hulls
Author: James M. Shoemaker
Publisher:
Total Pages: 530
Release: 1934
Genre: Planing hulls
ISBN:

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This report presents towing tests made in the N.A.C.A. tank of a parent form and five variations of a flying-boat hull. The beams of two of the dervied forms were made the same as that of the parent and the lengths changed by increasing and decreasing the spacing of stations. The lengths of two other of the derived forms were made the same as that of the parent while the beams were changed by increasing and decreasing the spacing of buttocks, all other widths being changed in proportion. The remaining derived form has the same length and beam as the parent, but the lines of the forebody were altered to give a planing bottom with no longitudinal curvature forward of the step.


Wartime Report

Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 222
Release:
Genre: Aeronautics
ISBN:

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Technical Note

Technical Note
Author:
Publisher:
Total Pages: 542
Release:
Genre: Aeronautics
ISBN:

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Hydrodynamic and Aerodynamic Tests of Models of Flying-boat Hulls Designed for Low Aerodynamic Drag

Hydrodynamic and Aerodynamic Tests of Models of Flying-boat Hulls Designed for Low Aerodynamic Drag
Author: Starr Truscott
Publisher:
Total Pages: 586
Release: 1938
Genre: Drag (Aerodynamics)
ISBN:

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N.A.C.A. models 74, 74-A, and 75 were tested in the N.A.C.A. tank to determine their hydrodynamic properties and in the N.A.C.A. 20-foot wind tunnel to determine their aerodynamic properties. The forms of these models were derived from that of a solid of revolution having a lowe air drag, and the departures from the form of this low-drag body were the minimum considered to give satisfactory take-off performance. Model 74 has a rounded bottom with flared chines, a transverse step wit ha small fairing aft of it, and a pointed afterbody. Model 74-A has the same forme except for the removal of the fairing aft of the step. Model 75 has a pointed step and a horizontal afterbody derived from the form of the N.A.C.A. model 35 series.