Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations /
by Kenneth P. Spreemann.

APA Citation

Spreemann, K. P., United States. National Aeronautics and Space Administration. (1959). Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations. Washington [D.C.]: National Aeronautics and Space Administration.

MLA Citation

Spreemann, Kenneth P, and United States. National Aeronautics and Space Administration. Design Guide for Pitch-up Evaluation And Investigation At High Subsonic Speeds of Possible Limitations Due to Wing-aspect-ratio Variations. Washington [D.C.]: National Aeronautics and Space Administration, 1959.