Report, 6th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1920.
Publication Title:
Report, 6th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1920.
Display Title:
Report, 6th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1920.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1921
Publish Date ISO Format:
1921-01-01T00:00:00Z
Publication Start:
19210101
Publication End:
19211231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1921
Description:
[1]+717 p. il. 14 pl. 30 p. of pl. 4°
Notes:
[Technical reports 83-110 are included in this annual report. Each report is also published separately in advance.]
Notes:
[Technical reports 83-110 are included in this annual report. Each report is also published separately in advance.] * For Sale by Superintendent of Documents. Paper. $1.50.
Notes:
CONTENTS.—Annual report.—Report S3. Wind tunnel studies in aerodynamic phenomena at high speed, by P. W. Caldwell and E. N. Fales: [with notes by George de Bothezat]. —Report 84. Data on design of plywood for aircraft: by Armin Elmendorf. —Report 85. Moisture resistant finishes for airplane woods: by M. E. Dunlap.— Report 86. Properties of special types of radiators: by S. R. Parsons.—Report 87. Effects of nature of cooling surface on radiator performance: by S. R. Parsons and R. V. Kleinsclimidt.—Report 88. Pressure drop in radiator air tubes; by S. R. Parsons. —Report 89. Comparison of alcogas aviation fuel with export aviation gasoline: by V. R. Gage. S. W. Sparrow, and D. R. Harper. 3d.—Report 90. Comparison of Hecter fuel with export aviation gasoline: by H. C. Dickinson. V. It. Case, and S.. Sparrow.-Report ill. Nomenclature for aeronautics: by National Advisory Committee for Aeronautics.-Report 02. Analysis of wing truss stresses, including effect of redundancies: by E. P. Warner and R. G. Miller.-Report 0:!. Aerodynamic characteristics of aerofoils; by National Advisory Committee for Aeronautics.-Report 04. Efficiency of small bearings in instruments of type used in aircraft; by P. II. Norton.-Report 95. Diagrams of airplane stability, by 11. Bateman: [with appendix to Report SO, Stability of parachute and helicopter].-Report 0(1. Statical longitudinal stability of airplanes: by Edward P. Warner.-Report 07. General theory of steady motion of airplane: by George de Bothezat.-Report OS. Design of wind tunnels and wind tunnel propellers, 2-; by P. II. Norton and Edward P. Warner.-Report 00. Accelerations in flight: by F. II. Norton anil E. T. Allen.-Report 100. Accelorometor design: by P. II. Norton and Edward P. Warner.-Report 101. Calculated performance of airplanes equipped with supercharging engines; by E. C. Kemble.-Report 102. Performance of liberty 12 airplane engine; by S. W. Sparrow and II. S. White.-Report 103. Performance of 300-horsepower Hispano-Suiza airplane engine: by S. W. Sparrow and II. S. White.-Report 104. Torsion of wing trusses at diving speeds; by Roy G. .Miller.-Report 105. Angles of attack and air speeds during maneuvers; by E. P. Warner and P. II. Norton.-Report 100. Turbulence in air tubes of radiators for aircraft engines: by S. R. Parsons.-Report 107. Highspeed engine pressure indicator of balanced diaphragm type; by II. C. Dickinson and P. B. Newell.-Report 10S. Some factors of airplane engine performance; by Victor R. (age.-Report 100. Experimental research on air propellers. 4: by W. P. Durand and E. P. Lesley.-Report 110. Altitude effect on air speed indicators; by Mayo I). Hersey, Pranklin L. Hunt, and Herbert N. Eaton.
Availability:
* For Sale by Superintendent of Documents. Paper. $1.50.