Technical notes. 3843. Experimental steady-state yawing derivatives of 60° delta-wing model as affected by changes in vertical position of wing and in ratio of fuselage diameter to wing span [with list of references]; by Byron M. Jaquet and Herman S. Fletcher.
Publication Title:
Experimental steady-state yawing derivatives of 60° delta-wing model as affected by changes in vertical position of wing and in ratio of fuselage diameter to wing span [with list of references]; by Byron M. Jaquet and Herman S. Fletcher.
Display Title:
Technical notes. 3843. Experimental steady-state yawing derivatives of 60° delta-wing model as affected by changes in vertical position of wing and in ratio of fuselage diameter to wing span [with list of references]; by Byron M. Jaquet and Herman S. Fletcher.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Jaquet, Byron M. and Fletcher, Herman S.
Date:
Oct. 1956
Publish Date ISO Format:
1956-10-01T00:00:00Z
Publication Start:
19561001
Publication End:
19561031
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
3
Publication year:
1956
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 20 p.+ [3] leaves, il. 4°
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.]
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.] † Distribution Made by Issuing Office.