Opening book details…
About this nonfiction
Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-propelled Airplane Model Having No Horizontal Tail by Parks, James H. 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
- Parks, James H.
- Publisher
- National Advisory Committee for Aeronautics, 1955.
- Published
- 1955
- Language
- EN
- Category
- nonfiction
More by Parks, James H.
Browse all works by Parks, James H.
Similar books
- Aerodynamic Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Configuration Having a Diamond-plan-form Wing Aspect Ration 3.08 and a Low, Swept Horizontal Tail — Alan B. Kehlet (1954)
- Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2° delta wing and an unswept horizontal tail. — Alan B. Kehlet (1958)
- Longitudinal Stability and Trim of Two Rocket-propelled Airplane Models Having 45° Sweptback Wings and Tails with the Horizontal Tail Mounted in Two Positions — James H. Parks (1953)
- Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 / John C. McFall, Jr. — McFall, John C. (1954)
- Flight Measurements of Aerodynamic Loads on the Horizontal Tail Surface of a Fighter-type Airplane — John B. Garvin (1947)
- 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)