Report. Aeronautics, 8th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1922, including Technical reports 133-158.
Publication Title:
Report. Aeronautics, 8th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1922, including Technical reports 133-158.
Display Title:
Report. Aeronautics, 8th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1922, including Technical reports 133-158.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1923
Publish Date ISO Format:
1923-01-01T00:00:00Z
Publication Start:
19230101
Publication End:
19231231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1923
Description:
ix+708 p. il. 4 pl. 1 tab. 4°
Notes:
[Each report is also published separately in advance.]
Notes:
[Each report is also published separately in advance.] * For Sale by Superintendent of Documents. Paper, $1.50.
Notes:
CONTENTS.—8th annual report.—Report 133. Tail piano; by Max M. Munk.—Report 134. Performance of Maybach 300-horsepower airplane engine; by S. W. Sparrow.—Report 135. Performance of B. M. W. 185-horsepower airplane engine; by S. W. Sparrow.—Report 136. Damping coefficients due to tail surfaces in aircraft, by Lynn Chu; condensed and modified by Edward P. Warner.—Report 137. Point drag and total drag of Navy struts no. 1 modified; by A. F. Zahm, R. H. Smith, and G. C. Hill.—Report 138. Drag of C class airship hull with varying length of cylindric midships; by A. F. Zahm, R. H. Smith, and G. C. Hill.—Report 139. Influence of model surface and air flow texture on resistance of aerodynamic bodies; by A. F. Zahm.—Report 140. Lift and drag effects of wing-tip rake; by A. F. Zahm, R. M. Bear, and G. C. Hill.—Report 141. Experimental research on air propellers, 5; by W. F. Durand and E. P. Lesley.—Report 142. General theory of thin wing sections [with list of references]; by Max M. Munk.—Report 143. Analysis of stresses in Gorman airplanes [with bibliography]; by Wilhelm Hoff.—Report 144. Decay of simple eddy; by H. Bateman.—Report 145. Internal stresses in laminated construction; by A. L. Heim, A. C. Knauss, and Louis Seutter.—Report 146. Six-component wind balance; by A. F. Zahm.—Report 147. Standard atmosphere; by Willis Ray Gregg.—Report 148. Pressure distribution over horizontal tail surfaces of airplane, 3; by F. H. Norton and W. G. Brown.—Report 149. Pressure distribution over rudder and fin of airplane in flight; by F. H. Norton and W. G. Brown.—Report 150. Pressure distribution over thick airfoils, model tests [with bibliography]; by F. H. Norton and D. L. Bacon.—Report 151. General biplane theory [with list of references]; by Max M. Munk.—Report 152. Aerodynamic properties of thick airfoils. 2, (continuation of Report 75); by F. H. Norton and D. L. Bacon.—Report 153. Controllability and maneuverability of airplanes; by F. H. Norton and W. G. Brown.—Report 154. Study of taking off and landing an airplane; by T. Carroll.—Report 155. Study of airplane maneuvers with special reference to angular velocities [with bibliography]; by H. J. E. Reid.—Report 156. Altitude effect on air speed indicators, 2 [with bibliography], (continuation of Report 110); by H. N. Eaton and W. A. MacNair.—Report 157. Nomenclature for aeronautics; [revision of Report 91].—Report 158. Mathematical equations for heat conduction in fins of air-cooled engines; by D. R. Harper, 3d, and W. B. Brown.
Availability:
* For Sale by Superintendent of Documents. Paper, $1.50.