Opening book details…
About this nonfiction
Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile 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 Aeronautics and Space Administration, 1960.
- Published
- 1960
- Language
- EN
- Category
- nonfiction
More by Schult, Eugene D.
Browse all works by Schult, Eugene D.
Similar books
- Some Effects of External Wing Tip Stores on the Rolling Effectiveness and Drag of Plain and Half-delta Tip Ailerons on a 4-Percent-thick Tapered, Unswept Wing — Roland D. English (1954)
- Drag Due to Lift at Mach Numbers Up to 2.0 — Edward C. Polhamus (1953)
- 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 — Eugene D. Schult (1955)
- Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60° delta wing at Mach numbers of 1.41, 1.62, and 1.96 — Odell A. Morris (1953)
- Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control — A. B. Blair (1978)
- Free-flight Measurements of the Rolling Effectiveness and Drag of Trailing-edge Spoilers on a Tapered Sweptback Wing at Mach Numbers Between 0.6 and 1.4 — Eugene D. Schult (1954)