Author: Raymond D. VoglerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 88
Book Description
Interference Effects of Single and Multiple Round Or Slotted Jets on a VTOL Model in Transition
Author: Raymond D. VoglerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 88
Book Description
Ground Effects on Single- and Multiple-jet VTOL Models at Transition Speeds Over Stationary and Moving Ground Planes (vertical Take-off and Landing)
Author: Raymond D. VoglerPublisher:
ISBN:
Category : Ground-effect machines
Languages : en
Pages : 66
Book Description
NASA Technical Note
Author: Free-stream Interference Effects on Effectiveness of Control Jets Near the Wing Tip of a VTOL Aircraft Model
Author: Kenneth P. SpreemannPublisher:
ISBN:
Category : Jets
Languages : en
Pages : 68
Book Description
Conference on V/STOL and STOL Aircraft, Ames Research Center, Moffett Field, California, April 4-5, 1966
Author: Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 486
Book Description
Manned Operations for the Apollo Lunar Module in a Simulated Space Environment
Author: O. L. PearsonPublisher:
ISBN:
Category : Extravehicular space suits
Languages : en
Pages : 920
Book Description
Simulated space environment performance tests of Apollo lunar module in thermal vacuum environment.
Longitudinal and Lateral Stability Characteristics of Two Four-jet Vtol Models in the Transition Speed Range
Author: Raymond D. VoglerPublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 132
Book Description
Analysis of a Jet in a Subsonic Crosswind
Author: Induces Velocity Field of a Jet in a Crossflow
Author: Richard L. FearnPublisher:
ISBN:
Category : Jets
Languages : en
Pages : 156
Book Description
An experimental investigation of a subsonic round jet exhausting perpendicularly from a flat plate into a subsonic crosswind of the same temperature was conducted. Velocity and pressure measurements were made in planes perpendicular to the path of the jet for ratios of jet velocity to crossflow velocity ranging from 3 to 10. The results of these measurements are presented in tabular and graphical forms. A pair of diffuse contrarotating vortices is identified as a significant feature of the flow, and the characteristics of the vortices are discussed.
NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 670
Book Description