WIND-TUNNEL INVESTIGATION OF A RAM-JET MISSILE MODEL HAVING A WING AND CANARD SURFACES OF DELTA PLAN FORM WITH 70 SWEPT LEADING EDGES. FORCE AND MOMENT CHARACTERISTICS AT COMBINED ANGLES OF PITCH AND SIDESLIP FOR MACH NUMBER 2.01

Driver, Cornelius; Hamilton, Clyde V.

WIND-TUNNEL INVESTIGATION OF A RAM-JET MISSILE MODEL HAVING A WING AND CANARD SURFACES OF DELTA PLAN FORM WITH 70 SWEPT LEADING EDGES. FORCE AND MOMENT CHARACTERISTICS AT COMBINED ANGLES OF PITCH AND SIDESLIP FOR MACH NUMBER 2.01

Active / Technical Report | Accession Number: AD0092213 | Open PDF

Abstract:

No Abstract Identified

Author(s):

Driver, Cornelius ; Hamilton, Clyde V.

Author Organization(s):

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Pagination:

0070

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

Distribution Statement:

Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

NACA-RM-L56B21

Monitor Series:

NASA

Subject Terms

Joint Capability Areas:

JCA_3_Force Application; JCA_3.1.1_Maneuver to Engage; JCA_3.1_Maneuver; JCA_7.2.1_Mitigate Lethal Effects; JCA_7.2_Mitigate; JCA_7_Protection; JCA_3.2_Engagement; JCA_3.2.1_Kinetic Means; JCA_5_Command and Control; JCA_5.3_Planning; JCA_6.4.1_Secure Information Exchange; JCA_6.4_Information Assurance; JCA_6_Net Centric

Modernization Areas:

Autonomy

Communities of Interest:

Weapons Technologies

Descriptor(s):

*GUIDED MISSILES, *SWEPT WINGS, *SUPERSONIC FLOW, *RAMJET TEST VEHICLES, *CANARD CONFIGURATIONS, CONTROL SYSTEMS, WIND TUNNEL TESTS, SIDESLIP, MODEL TESTS, PITCH(INCLINATION)

Field(s)/Group(s):

Guided Missile Dynamics, Configurations and Control Surfaces

Report Date:

1956 Apr 26