SINGLE-HOLE, STAGNATION-POINT, MASS INJECTION FROM ZERO TO 20 DEGREE AOA

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$50,000.00
Award Year:
1983
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Award Id:
224
Agency Tracking Number:
224
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
1560 Brookhollow Driving, Santa Ana, CA, 92705
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
() -
Business Contact:
James Elliot Dunn
(714) 556-2800
Research Institute:
n/a
Abstract
MEASUREMENTS OF TEMPERATURE AND PRESSURE HAVE BEEN MADE ON TWO MODELS WITH STAGNATION-POINT, SINGLE-HOLE, MASS INJECTION RATIOS FROM ZERO TO 99 AND AT 0, 5, 10, AND 20 DEGREES ANGLE-OF-ATTACK IN THE NASA LANGLEY 8' HIGH TEMPERATURE-STRUCTURES-TUNNEL. THESE RAW-DATA HAVE NOT BEEN REDUCED TO NONDIMENSIONAL PAID-MECHANIC SIMILARITY PARAMETERS SO THAT THE DATA CAN BE USED FOR DESIGN PURPOSES IN THE GENERAL ICBM REENTRY ENVIRONMENT. THE PROPOSAL HEREIN IS TO REDUCE THE AVAILABLE TEST DATA TO STANTON NUMBER, COOLANT-EFFICIENCY, PRESSURE COEFFICIENT AND OTHER RELEVANT SIMILARITY PARAMETERS SO THAT DESIGNERS AND ANALYSTS CAN USE THE TEST RESULTS TO DESIGN GAS-COOLED TUNGSTEN NON-SETIPS FOR BRV'S, AND POSSIBLY SATELLITE REENTRY VEHICLES.

* information listed above is at the time of submission.

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