Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462
Book Description
NACA-University Conference on Aerodynamics, Construction, and Propulsion
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462
Book Description
NACA-University Conference on Aerodynamics, Construction, and Propulsion
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 878
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 878
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1194
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1194
Book Description
Examination of the Existing Data on the Heat Transfer of Turbulent Boundary Layers at Supersonic Speeds from the Point of View of Reynolds Analogy
Author: Alvin Seiff
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 654
Book Description
Heat-transfer data from four wind-tunnel experiments and two free-flight experiments with turbulent boundary layers have been examined to see whether or not they are well represented by the Reynolds analogy or a modification thereof. The heat-transfer results are put into the form of dimensionless Stanton numbers based on fluid properties at the outer edge of the boundary layer and are compared with skin-friction coefficients for the same Mach numbers and wall to free-stream temperature ratios as obtained from an interpolation of the existing skin-friction data. The effective Reynolds number is taken to be the length Reynolds number measured from the effective turbulent origin, a position which differs importantly from the leading edge of the test surface in some cases.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 654
Book Description
Heat-transfer data from four wind-tunnel experiments and two free-flight experiments with turbulent boundary layers have been examined to see whether or not they are well represented by the Reynolds analogy or a modification thereof. The heat-transfer results are put into the form of dimensionless Stanton numbers based on fluid properties at the outer edge of the boundary layer and are compared with skin-friction coefficients for the same Mach numbers and wall to free-stream temperature ratios as obtained from an interpolation of the existing skin-friction data. The effective Reynolds number is taken to be the length Reynolds number measured from the effective turbulent origin, a position which differs importantly from the leading edge of the test surface in some cases.
Structures Technology
Author: Ahmed Khairy Noor
Publisher: AIAA
ISBN: 9781563471162
Category : Technology & Engineering
Languages : en
Pages : 544
Book Description
Drawn from early volumes of Aerospace America and its antecedents, this book rescues the insights, concerns, and dreams of dozens of structural engineers for the next generation of aerospace scientists and engineers. Written by eminent individuals in structures, this book provides accessible source material for university-level design courses in aerospace engineering. The first paper in Structures Technology deals with new structures for future aerospace systems and provides a contrast between our current thinking and past technology plans. Succeeding papers are historical reports covering materials and structures, general structures technology, aircraft structures, space structures, and structural dynamics technology. You will also find sections covering structural configurations, thermal protection systems, subsonic aircraft, supersonic and hypersonic vehicles and structures for space systems.
Publisher: AIAA
ISBN: 9781563471162
Category : Technology & Engineering
Languages : en
Pages : 544
Book Description
Drawn from early volumes of Aerospace America and its antecedents, this book rescues the insights, concerns, and dreams of dozens of structural engineers for the next generation of aerospace scientists and engineers. Written by eminent individuals in structures, this book provides accessible source material for university-level design courses in aerospace engineering. The first paper in Structures Technology deals with new structures for future aerospace systems and provides a contrast between our current thinking and past technology plans. Succeeding papers are historical reports covering materials and structures, general structures technology, aircraft structures, space structures, and structural dynamics technology. You will also find sections covering structural configurations, thermal protection systems, subsonic aircraft, supersonic and hypersonic vehicles and structures for space systems.
Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Vortex Interference on Slender Airplanes
Author: Alvin H. Sacks
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 702
Book Description
It is found that the impulse of each shed vortex and its image vortex in a transformed circle plane enters into all the interference forces and moments on the airplane. A simple theorem is given for the interference forces in steady straight flight which are found to depend on this impulse evaluated only at the wing trailing edge and at the base of the configuration.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 702
Book Description
It is found that the impulse of each shed vortex and its image vortex in a transformed circle plane enters into all the interference forces and moments on the airplane. A simple theorem is given for the interference forces in steady straight flight which are found to depend on this impulse evaluated only at the wing trailing edge and at the base of the configuration.
NASA Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66
Book Description
WADC Technical Report
Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1540
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1540
Book Description