Pitching-Moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-Delta-Wing and Slender-Body Combination and Approximate Solutions for Broad-Delta-Wing and Slender-Body Combinations
Abstract
The pitching-moment derivatives Cmq and Cma at supersonic speeds are developed for a slender-delta-wing and slender-body combination having no afterbody. By drawing an analogy between the aerodynamics of the wing-body section of the combination and the aerodynamics of a delta wing alone, the results for the slender-delta-wing and slender-body combination are modified to the extent that approximate solutions for Cmq and for broad-delta-wing and slender-body combinations can be obtained.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1951
- Accession Number
- ADA380293
Entities
People
- Arthur Henderson Jr.
Organizations
- National Aeronautics and Space Administration