Longitudinal Stability and Control Characteristics of a Semispan Airplane Model with a Swept-Back Tail from Tests at Transonic Speeds by the NACA Wing-Flow Method
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 28, 1947
- Accession Number
- ADA800829
Entities
People
- John A. Zalovcik
- Richard H. Sawyer
Organizations
- Langley Research Center