Author: Joseph Kaye
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 23
Book Description
An Inexpensive Supersonic Wind Tunnel for Heat-transfer Measurements
Author: Joseph Kaye
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 23
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 23
Book Description
AN INEXPENSIVE SUPERSONIC WIND TUNNEL FOR HEAT-TRANSFER MEASUREMENTS. PART 1. APPARATUS, DATA, AND RESULTS FOR A LAMINAR BOUNDARY LAYER BASED ON A SIMPLE ONE-DIMENSIONAL FLOW MODEL.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Design of a Small Supersonic Wind Tunnel for Heat Transfer Measurements at Mach Five
Author: Peter Ashurkoff
Publisher:
ISBN:
Category :
Languages : en
Pages : 170
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 170
Book Description
Design of an Inexpensive Supersonic Wind Tunnel with an Inlet Mach Number of Five for Heat Transfer Studies
Author: John Russell Radbill
Publisher:
ISBN:
Category :
Languages : en
Pages : 88
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 88
Book Description
Hydraulic Research in the United States
Author:
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 230
Book Description
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 230
Book Description
Heat Transfer Measurements Using Narrow-band Liquid Crystals in a Supersonic Blowdown Wind Tunnel
Author: Hsieh-Hsiang Sam Chiu
Publisher:
ISBN:
Category : Heat
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages :
Book Description
Report
Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 232
Book Description
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 232
Book Description
Supersonic and Subsonic Wind Tunnel Heat-Transfer Measurements in the Base Cavity Region of the Shuttle Solid Rocket Booster During Simulated Reentry
Author: W. R. Hawkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Tests were conducted on the aft section of the Space Shuttle Solid Rocket Booster at Mach numbers 3.75 and 0.5 at selected angles of attack from 90-180 deg simulating reentry attitudes. The tests wre conducted in the AEDC Supersonic Wind Tunnel A to obtain heat-transfer coefficients in the base cavity region. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Tests were conducted on the aft section of the Space Shuttle Solid Rocket Booster at Mach numbers 3.75 and 0.5 at selected angles of attack from 90-180 deg simulating reentry attitudes. The tests wre conducted in the AEDC Supersonic Wind Tunnel A to obtain heat-transfer coefficients in the base cavity region. (Author).
NBS Special Publication
Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 226
Book Description
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 226
Book Description
National Bureau of Standards Miscellaneous Publication
Author:
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 220
Book Description
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 220
Book Description