Opening book details…
About this nonfiction
A Free-flight Investigation at High Subsonic and Low Supersonic Speeds of the Rolling Effectiveness and Drag of Three Spoiler Controls Having Potentially Low Actuating-force Requirements by Schult, Eugene D. is a nonfiction available to read on EtoBox.
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Schult, Eugene D.
- Publisher
- National Advisory Committee for Aeronautics, 1955.
- Published
- 1955
- Language
- EN
- Category
- nonfiction
More by Schult, Eugene D.
Browse all works by Schult, Eugene D.
Similar books
- The Problem of Roughness Drag at Supersonic Speeds — K. R. Czarnecki (1966)
- Pressure Distributions for a Rectangular Supersonic Inlet at Subsonic Speeds — Dennis E. Fuller (1976)
- Flight Measurements of Lifting Pressures for a Thin Low-aspect-ratio Wing at Subsonic, Transonic, and Low Supersonic Speeds — Thomas A. Byrdsong (1977)
- Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds — Lomax, Harvard. (1953)
- A Method for Designing Low-drag Nose-inlet-body Combinations for Operation at Moderate Supersonic Speeds — Robert R Howell; Langley Aeronautical Laboratory.; United States. National Adviosry Committee for Aeronautics (1954)
- Correspondence Flows for Wings in Linearized Potential Fields at Subsonic and Supersonic Speeds — Sidney M. Harmon (1951)