Author: Warren Jr GillespiePublisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Lift, Drag, and Longitudinal Stability at Mach Numbers from 0.8 to 2.1 of a Rocket-powered Model Having a Tapered Unswept Wing of Aspect Ratio 3 and Inline Tail Surfaces
Author: Warren Jr GillespiePublisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces
Author: Warren Jr GillespiePublisher:
ISBN:
Category :
Languages : en
Pages : 29
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Aero/space Engineering
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 988
Book Description
Aeronautical Engineering Review
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1846
Book Description
Drag Due to Lift at Mach Numbers Up to 2.0
Author: Edward C. PolhamusPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28
Book Description
Longitudinal Stability and Drag Characteristics at Mach Numbers from 0.70 to 1.37 of Rocket-propelled Models Having a Modified Triangular Wing
Author: Rowe Jr ChapmanPublisher:
ISBN:
Category :
Languages : en
Pages : 35
Book Description
Comparison of Low-lift Drag at Mach Numbers from 0.74 to 1.37 of Rocket-boosted Models Having Externally Braced Wings and Cantilever Wings
Author: Waldo L. DickensPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 22
Book Description
An investigation has been conducted to determine whether the low-lift drag of a rocket-model airplane-like configuration could be reduced at transonic and low supersonic Mach numbers by reducing the wing thickness while external braces were used to provide the necessary bending strength. The investigation consisted of flight training two rocket models having aspect ratio 3.04, unswept braced tapered wings mounted on fuselages with the same fineness ratios and cross-sectional area distributions. Data collected from the flight test of a model having a thicker cantilever wing of the same plan form were compared with data collected in this investigation.
Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6
Author: John D. MorrowPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58
Book Description
