Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
3 results returnedSearch results
- Contributions of wing, tail, and fuselage to the aerodynamic characteristics of a semispan model of a supersonic airplane configuration at transonic speeds from tests by the NACA wing-flow method
- Investigation of the Distribution of Lift, Drag, and Pitching Moment Between the Wing and Fuselage of a 1/30-Scale Semispan Model of the Bell X-5 Airplane at a Mach Number of 1.24 by the NACA Wing-Flow Method
- Landing conditions for large airplanes in routine operations