Showing 1 - 20 results of 24 for search 'Von Doenhoff, Albert E.', query time: 0.07s
Refine Results
-
1
A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition / by Von Doenhoff, Albert E.
Published 1956Call Number: Loading…
Located: Loading…Government Document Book Loading… -
2
An analysis of the power-off landing maneuver in terms of the capabilities of the pilot and the aerodynamic characteristics of the airplane / by Von Doenhoff, Albert E.
Published 1953Call Number: Loading…
Located: Loading…Government Document Book Loading… -
3
Studies of the use of Freon-12 as a wind-tunnel testing medium / by Von Doenhoff, Albert E.
Published 1953Call Number: Loading…
Located: Loading…Government Document Book Loading… -
4
Determination of general relations for the behavior of turbulent boundary layers / by Von Doenhoff, Albert E.
Published 1943Call Number: Loading…
Located: Loading…Government Document Book Loading… -
5
Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel / by Von Doenhoff, Albert E.
Published 1944Call Number: Loading…
Located: Loading…Government Document Book Loading… -
6
An application of the von Ká́rmán-Millikan laminar boundary-layer theory and comparison with experiment / by Von Doenhoff, Albert E.
Published 1935Call Number: Loading…Online Access
Located: Loading…
Government Document eBook -
7
A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient / by Von Doenhoff, Albert E.
Published 1938Call Number: Loading…
Located: Loading…Government Document Book Loading… -
8
Tests of a 0.1475c aileron with a tab on low-drag section for Curtiss XP-60 airplane in the low-turbulence tunnel / by Von Doenhoff, Albert E.
Published 1941Call Number: Loading…
Located: Loading…Government Document Book Loading… -
9
Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil / by Von Doenhoff, Albert E.
Published 1942Call Number: Loading…
Located: Loading…Government Document Book Loading… -
10
Investigation of the boundary layer about a symmetrical airfoil in a wind tunnel of low turbulence / by Von Doenhoff, Albert E.
Published 1940Call Number: Loading…
Located: Loading…Government Document Book Loading… -
11
Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company / by Von Doenhoff, Albert E.
Published 1944Call Number: Loading…
Located: Loading…Government Document Book Loading… -
12
Preliminary investigation in the NACA low-turbulence tunnel of low-drag airfoil sections suitable for admitting air at the leading edge / by Von Doenhoff, Albert E.
Published 1942Call Number: Loading…
Located: Loading…Government Document Book Loading… -
13
A method of rapidly estimating the position of the laminar separation point / by Von Doenhoff, Albert E.
Published 1938Call Number: Loading…Online Access
Located: Loading…
Government Document eBook -
14
A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient / by Von Doenhoff, Albert E.
Published 1938Call Number: Loading…Online Access
Located: Loading…
Government Document eBook -
15
An application of the von Kármán-Millikan laminar boundary-layer theory and comparison with experiment / by Von Doenhoff, Albert E.
Published 1935Call Number: Loading…
Located: Loading…Government Document Book Loading… -
16
Low-speed test of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers / by Von Doenhoff, Albert E.
Published 1947Call Number: Loading…
Located: Loading…Government Document Book Loading… -
17
The Langley two-dimensional low-turbulence pressure tunnel / by Von Doenhoff, Albert E.
Published 1947Call Number: Loading…
Located: Loading…Government Document Book Loading… -
18
Note of similarity conditions for flows with heat transfer / by Von Doenhoff, Albert E.
Published 1948Call Number: Loading…Search for the full-text version of this title in HathiTrust
Located: Loading…
Government Document Book -
19
A Method of rapidly estimating the position of the laminar separation point / by Von Doenhoff, Albert E.
Published 1938Call Number: Loading…
Located: Loading…Government Document Book Loading… -
20
Formulas for use in boundary-layer calculations on low-drag wings / by Jacobs, Eastman N. (Eastman Nixon), 1902-1987
Published 1941Other Authors: “…Von Doenhoff, Albert E.…”
Call Number: Loading…
Located: Loading…Government Document Book Loading…
Search Tools:
RSS Feed
Related Subjects
Aerofoils
Charts, diagrams, etc
Boundary layer
Wind tunnel testing
Drag (Aerodynamics)
Testing
Aerodynamic load
Airplanes
Aeronautics
Aerodynamics
Air flow
Laminar boundary layer
Research
Reynolds number
Wings
Flight testing
Fluid dynamics
Laminar flow
Lift (Aerodynamics)
Mathematics
Wind tunnels
Ailerons
Aircraft
Aircraft accidents and safety
Aircraft construction
Aircraft engines
Aircraft parts
Angle of attack (Aerodynamics)
Autogiros
Boundary layer control