Opening book details…
About this nonfiction
Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° by Foster, Gerald V. 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
- Foster, Gerald V.
- Publisher
- National Aeronautics and Space Administration, 1960.
- Published
- 1960
- Language
- EN
- Category
- nonfiction
More by Foster, Gerald V.
Browse all works by Foster, Gerald V.
Similar books
- Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75° — Spearman, M. Leroy. (1959)
- Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75° — Gerald V. Foster (1960)
- Longitudinal Aerodynamic Characteristics at Transonic Speeds of a V/STOL Airplane Configuration with a Fixed Delta Wing Having Auxiliary Variable-sweep Outboard Panels — Arvo A. Luoma (1961)
- Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.40 to 1.10 of a Blunted Right-trangular Pyramidal Lifting Reentry Configuration Employing Variable-sweep Wing Panels by Bernard Spencer, Jr. — Spencer, Bernard. (1963)
- Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-wing-sweep STOL Configuration — Gerald V. Foster (1960)
- Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108° — Ross B. Robinson (1960)