Technical notes. 3243. Theoretical analysis of an airplane acceleration restrictor controlled by normal acceleration, pitching acceleration, and pitching velocity [with list of references]; by Christopher C. Kraft, jr.
Publication Title:
Theoretical analysis of an airplane acceleration restrictor controlled by normal acceleration, pitching acceleration, and pitching velocity [with list of references]; by Christopher C. Kraft, jr.
Display Title:
Technical notes. 3243. Theoretical analysis of an airplane acceleration restrictor controlled by normal acceleration, pitching acceleration, and pitching velocity [with list of references]; by Christopher C. Kraft, jr.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Kraft, Christopher C. jr.
Date:
Sept. 1954
Publish Date ISO Format:
1954-09-01T00:00:00Z
Publication Start:
19540901
Publication End:
19540930
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
4
Publication year:
1954
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 42 p.+[2] p. 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.