Local Flow Field Around a Pylon-mounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7 PDF Download

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Local Flow Field Around a Pylon-mounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7

Local Flow Field Around a Pylon-mounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7 PDF Author: Frank W. Burcham
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 66

Book Description

Local Flow Field Around a Pylon-mounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7

Local Flow Field Around a Pylon-mounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7 PDF Author: Frank W. Burcham
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 66

Book Description

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 574

Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 448

Book Description

Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R)

Flight-test Results from Two Total Temperature Probes for Air-data Measurements Up to 2014 ̊K (3625 ̊R) PDF Author: Jack Nugent
Publisher:
ISBN:
Category : Fluidic devices
Languages : en
Pages : 60

Book Description
An experimental temperature probe package containing a fluidic oscillator temperature probe and a shielded thermocouple temperature probe was tested during several X-15 flights. The X-15 flights provided greatly varying test conditions, including a wide range of rapidly changing total temperatures and Mach numbers which extended from subsonic to hypersonic speeds. Within restricted ranges of free-stream Mach number, free-stream unit weight flow, and local stagnation pressure, both probes yielded ramp outputs of temperature parallel to ramp inputs of free-stream total temperature. Within these ranges both probes were used to determine total temperature in the Mach 6 temperature environment. Because ambient temperature was known, both probes were used to estimate velocity and Mach number.

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1250

Book Description

Propulsion Flight Research at NASA Dryden From 1967 to 1997

Propulsion Flight Research at NASA Dryden From 1967 to 1997 PDF Author: Frank W. Burcham (Jr.)
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

Book Description

Flight-measured Aerodynamic Drag of Two Large External Tanks Attached to the X-15-2 Airplane at Mach Numbers of 1.6 to 2.3

Flight-measured Aerodynamic Drag of Two Large External Tanks Attached to the X-15-2 Airplane at Mach Numbers of 1.6 to 2.3 PDF Author: David F. Fisher
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 20

Book Description

Hypersonics Before the Shuttle: A Concise History of the X-15 Research Airplane

Hypersonics Before the Shuttle: A Concise History of the X-15 Research Airplane PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 134

Book Description

Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7

Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7 PDF Author: R. H. Roberts
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 150

Book Description
Experimental data were obtained to aid in the prediction of aerodynamic loads and separation-trajectory characteristics on stores under the influence of an aircraft flow field. Four types of data were obtained in the vicinity of a generalized aircraft model: (1) flow field surveys, using a 40-deg cone probe, to determine the local velocity field, (2) force and moment data on four store models, (3) pressure distribution data on an ogive-cylinder model, and (4) captive-trajectory store separation data on one store model. The generalized aircraft model consisted of a swept-wing/fuselage combination with rectangular, flow-through engine ducts.

Hypersonic Aerothermodynamics

Hypersonic Aerothermodynamics PDF Author: John J. Bertin
Publisher: AIAA
ISBN: 9781563470363
Category : Science
Languages : en
Pages : 644

Book Description
A modern treatment of hypersonic aerothermodynamics for students, engineers, scientists, and program managers involved in the study and application of hypersonic flight. It assumes an understanding of the basic principles of fluid mechanics, thermodynamics, compressible flow, and heat transfer. Ten chapters address: general characterization of hypersonic flows; basic equations of motion; defining the aerothermodynamic environment; experimental measurements of hypersonic flows; stagnation-region flowfield; the pressure distribution; the boundary layer and convective heat transfer; aerodynamic forces and moments; viscous interactions; and aerothermodynamics and design considerations. Includes sample exercises and homework problems. Annotation copyright by Book News, Inc., Portland, OR
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