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COMPUTATIONAL TECHNIQUE AND DESIGN GUIDE DEFINING DEPARTURE/SPIN RESISTANT…

Award Information

Agency:
Department of Defense 		Branch:
Air Force 		Award ID:
2106 		Program Year/Program:
1986 / SBIR
Agency Tracking Number:
2106 		Solicitation Year:
N/A 		Solicitation Topic Code:
N/A 		Solicitation Number:
N/A
Small Business Information
Bihrle Applied Research, Inc.
81 Research Dr Hampton, VA -
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Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 1986
Title: COMPUTATIONAL TECHNIQUE AND DESIGN GUIDE DEFINING DEPARTURE/SPIN RESISTANT FOREBODY CONFIGURATIONS DEVELOPMENT
Agency / Branch: DOD / USAF
Contract: N/A
Award Amount: $269,000.00
 

Abstract:

AIRPLANE FOREBODY DESIGN HAS CONSISTENTLY DEMONSTRATED SIGNIFICANT INFLUENCES ON BOTH STATIC AND ROTATIONAL AERODYNAMICS AND, CONSEQUENTLY, ON HIGH ANGLE-OF-ATTACK FLIGHT CHARACTERISTICS AND SPIN BEHAVIOR. AN EXTENSIVE HIGH ANGLE-OF-ATTACK DATA BASE FOR MILITARY CONFIGURATIONS HAS BEEN GENERATED USING THE ROTARY BALANCE AT THE NASA LANGLEY 20-FOOT SPIN TUNNEL. THIS DATA BASE WILL BE UTILIZED TO CORRELATE STATIC AND ROTATIONAL AERODYNAMIC CHARACTERISTICS WITH FOREBODY DESIGN PARAMETERS. THE RESULTS OF THIS ANALYSIS WILL BE FORMULATED INTO A PRELIMINARY DESIGN GUIDE, WHICH WILL DEMONSTRATE THE RELATIONSHIP OF HIGH ANGLE-OF-ATTACK AERODYNAMIC CHARACTERISTICS WITH FOREBODY DESIGN. THIS TYPE OF INFORMATION IS REQUIRED AS A PRE-REQUISITE FOR THE FORMULATION OF COMPUTATIONAL TECHNIQUES.

Principal Investigator:

Billy P Barnhart
5164330710

Business Contact:

Small Business Information at Submission:

Bihrle Applied Research Inc.
400 Jericho Turnpike Jericho, NY 11753

EIN/Tax ID:
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No