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Cilt sonuçları

A Benedictine Nun of Stanbrook, Stanbrook, Thomas A. Nelson · Yayınevi bilinmiyor

Sayfa sayısı yok · 1998-03

Kategori yok

AerodynamicsWind-tunnel Tests on the Stability and Drag of Some Blunt-nosed Bodies at High Subsonic Speeds by A.StanbrookA. Stanbrook

Wind-tunnel Tests on the Stability and Drag of Some Blunt-nosed Bodies at High Subsonic Speeds by A.Stanbrook

A. Stanbrook · Yayınevi bilinmiyor

Sayfa sayısı yok · 1968

Aerodynamics

DragA Correlation of the Forebody Drag of Cylinders with Plane and Hemispherical Noses at MACH Numbers from Zero to 2.5 by A.StanbrookA. Stanbrook

A Correlation of the Forebody Drag of Cylinders with Plane and Hemispherical Noses at MACH Numbers from Zero to 2.5 by A.Stanbrook

A. Stanbrook · Yayınevi bilinmiyor

Sayfa sayısı yok · 1987

Drag

Static stabilityAn Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 To1.8 by A.Stanbrook and M.D.DobsonA. Stanbrook

An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 To1.8 by A.Stanbrook and M.D.Dobson

A. Stanbrook · Yayınevi bilinmiyor

Sayfa sayısı yok · 1968

Static stability

Chant (Plain, Gregorian, etc.)A Grammar of Plainsong by a Benedictine of StanbrookStanbrook Abbey, A Benedictine of Stanbrook

A Grammar of Plainsong by a Benedictine of Stanbrook

Stanbrook Abbey, A Benedictine of Stanbrook · Yayınevi bilinmiyor

106 sayfa · 1934

Chant (Plain, Gregorian, etc.)

Gregorian chantsA Grammar of PlainsongA Benedictine of Stanbrook, Stanbrook Abbey

A Grammar of Plainsong

A Benedictine of Stanbrook, Stanbrook Abbey · Yayınevi bilinmiyor

128 sayfa · 1926

Gregorian chants

CiltExperimental Pressure Distributions on Combinations of a Cylindrical Body with Two Rectangular Wings at Mach Numbers of 1.42, 1.61 and 1.82A. Stanbrook

Experimental Pressure Distributions on Combinations of a Cylindrical Body with Two Rectangular Wings at Mach Numbers of 1.42, 1.61 and 1.82

A. Stanbrook · Yayınevi bilinmiyor

Sayfa sayısı yok · 1958

Kategori yok

Aerodynamics, TransonicExperimental pressure distributions on a plane - nosed cylinder at subsonic and transonic speedsA. Stanbrook

Experimental pressure distributions on a plane - nosed cylinder at subsonic and transonic speeds

A. Stanbrook · Yayınevi bilinmiyor

19 sayfa · 1966

Aerodynamics, Transonic

CiltThe Influence of a Model on Plenum Chamber Indication of Mach Number in a Slotted Wall Wind TunnelL. C. Squire

The Influence of a Model on Plenum Chamber Indication of Mach Number in a Slotted Wall Wind Tunnel

L. C. Squire · Yayınevi bilinmiyor

6 sayfa · 1958

Kategori yok

CiltA Wind-tunnel Investigation of the Directional and Longitudinal Stability of the Javelin Aircraft at Transonic Speeds, Including Comparison with Flight Test ResultsE. P. Sutton

A Wind-tunnel Investigation of the Directional and Longitudinal Stability of the Javelin Aircraft at Transonic Speeds, Including Comparison with Flight Test Results

E. P. Sutton · Yayınevi bilinmiyor

Sayfa sayısı yok · 1959

Kategori yok

CiltA Wind Tunnel Investigation of the Directional Stability of the Javelin Aircraft at Transonic Speeds, Including a Comparison with Flight Test ResultsE.P. Sutton

A Wind Tunnel Investigation of the Directional Stability of the Javelin Aircraft at Transonic Speeds, Including a Comparison with Flight Test Results

E.P. Sutton · Yayınevi bilinmiyor

54 sayfa · 1959

Kategori yok

CiltAn Experimental Study of the Glancing Interaction Between a Shock Wave and a Turbulent Boundary LayerBilinmeyen yazar

An Experimental Study of the Glancing Interaction Between a Shock Wave and a Turbulent Boundary Layer

Bilinmeyen yazar · Yayınevi bilinmiyor

8 sayfa · 1961

Kategori yok

CiltSome Experiments with and Without Connection Between the Upper and Lower Plenum Chambers of a Slotted Tunnel with an Open Area Ratio of 16 PercentD. A. Secomb

Some Experiments with and Without Connection Between the Upper and Lower Plenum Chambers of a Slotted Tunnel with an Open Area Ratio of 16 Percent

D. A. Secomb · Yayınevi bilinmiyor

Sayfa sayısı yok · 1967

Kategori yok

CiltEffects of Some Changes in Body Length and Nose Shape on the Aerodynamic Characteristics of Wing-body Combinations at Supersonic SpeedsS. Tomlin, A. Stanbrook

Effects of Some Changes in Body Length and Nose Shape on the Aerodynamic Characteristics of Wing-body Combinations at Supersonic Speeds

S. Tomlin, A. Stanbrook · Yayınevi bilinmiyor

10 sayfa · 1958

Kategori yok

CiltAn Experimental Study of an Upstream Support System in an Asymmetric Supersonic NozzleA. Stanbrook

An Experimental Study of an Upstream Support System in an Asymmetric Supersonic Nozzle

A. Stanbrook · Yayınevi bilinmiyor

Sayfa sayısı yok · 1963

Kategori yok

CiltWind Tunnel Tests on a Half Model of a Swept Wing Transport Aircraft (Vickers-Armstrong VC 10) at Mach Numbers from 0.4 to 0.96A. Stanbrook

Wind Tunnel Tests on a Half Model of a Swept Wing Transport Aircraft (Vickers-Armstrong VC 10) at Mach Numbers from 0.4 to 0.96

A. Stanbrook · Yayınevi bilinmiyor

49 sayfa · 1964

Kategori yok

CylindersA Correlation of the Forebody Drag of Cylinders with Plane and Hemispherical Noses at Mach Numbers from Zero to 2.5A. Stanbrook, Aeronautical Research Council (Great Britain)

A Correlation of the Forebody Drag of Cylinders with Plane and Hemispherical Noses at Mach Numbers from Zero to 2.5

A. Stanbrook, Aeronautical Research Council (Great Britain) · Yayınevi bilinmiyor

7 sayfa · 1964

Cylinders

AerodynamicsAn Experimental Investigation of the Aerodynamic Characteristics of Some Short Bodies, with Or Without Fins, at Mach NumbersA. Stanbrook

An Experimental Investigation of the Aerodynamic Characteristics of Some Short Bodies, with Or Without Fins, at Mach Numbers

A. Stanbrook · Yayınevi bilinmiyor

13 sayfa · 1968

Aerodynamics

CiltAn Investigation of the Static Stability and Drag of Two Conical Re-entry Heads at Mach Numbers from 0.4 to 1.8M. D. Dobson, A. Stanbrook

An Investigation of the Static Stability and Drag of Two Conical Re-entry Heads at Mach Numbers from 0.4 to 1.8

M. D. Dobson, A. Stanbrook · Yayınevi bilinmiyor

54 sayfa · 1966

Kategori yok

CiltAn Experimental Investigation of the Characteristics of Some Plane and Cambered 65 Degrees Delta Wings at Mach Numbers from 0.7 to 2.0L. C. Squire

An Experimental Investigation of the Characteristics of Some Plane and Cambered 65 Degrees Delta Wings at Mach Numbers from 0.7 to 2.0

L. C. Squire · Yayınevi bilinmiyor

110 sayfa · 1961

Kategori yok